Skipping 736 KB.. Full Log

Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Cd =  [[0.019540190626695868, 0.01741891163486496, 0.01637754544160998, 0.01572340736888129, 0.01529976634123639, 0.015051258605772694, 0.014977771651912143], [0.02003019062669587, 0.017828911634864962, 0.01673754544160998, 0.01606340736888129, 0.01561976634123639, 0.015351258605772694, 0.015267771651912142], [0.020570190626695867, 0.01826891163486496, 0.01712754544160998, 0.016423407368881288, 0.015949766341236387, 0.015671258605772693, 0.015577771651912143], [0.02114019062669587, 0.01873891163486496, 0.017547545441609982, 0.016813407368881286, 0.01631976634123639, 0.016011258605772693, 0.015907771651912143], [0.021770190626695867, 0.01924891163486496, 0.01800754544160998, 0.017233407368881286, 0.01671976634123639, 0.01639125860577269, 0.016267771651912143], [0.02246019062669587, 0.01980891163486496, 0.01850754544160998, 0.017693407368881288, 0.017139766341236387, 0.016801258605772692, 0.01665777165191214], [0.023210190626695867, 0.02041891163486496, 0.01904754544160998, 0.01819340736888129, 0.01760976634123639, 0.01724125860577269, 0.01707777165191214], [0.02425019062669587, 0.02125891163486496, 0.01979754544160998, 0.01887340736888129, 0.01824976634123639, 0.017851258605772694, 0.01765777165191214], [0.025430190626695867, 0.02221891163486496, 0.02063754544160998, 0.019653407368881288, 0.01897976634123639, 0.01853125860577269, 0.018307771651912143], [0.026710190626695867, 0.02324891163486496, 0.021547545441609983, 0.02048340736888129, 0.019759766341236388, 0.019271258605772692, 0.019007771651912142], [0.02810019062669587, 0.02435891163486496, 0.02252754544160998, 0.021383407368881287, 0.02058976634123639, 0.02006125860577269, 0.019757771651912143], [0.029590190626695868, 0.02554891163486496, 0.02357754544160998, 0.02233340736888129, 0.02148976634123639, 0.02090125860577269, 0.02055777165191214]]

real	4m41.071s
user	0m0.015s
sys	0m0.187s
+ status=0
+ set +x

=================================================
CAPS verification (using pyCAPS) case autoLink_Pytest.py passed (as expected)
=================================================


*************************************************
*************************************************

=================================================
Did not run examples for:

tsfoil
=================================================

All tests pass!


=================================================
Legacy Using python : /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/ESP/venv/Scripts/python
=================================================

Running.... LINEARAERO PyTests

=================================================
+ rm -rf avl_PyTest
+ echo 'avl_PyTest.py test;'
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
avl_PyTest.py test;
+ python -u avl_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Running AVL
CXtot   0.0006119078685747062
CYtot   -6.284473496001477e-15
CZtot   -0.3012861394886067
Cltot   -4.781528092304838e-14
Cmtot   -0.1945055953450459
Cntot   -2.340062347995671e-15
Cl'tot  -4.784883814335109e-14
Cn'tot  -1.505214228583796e-15
CLtot   0.3012509314150749
CDtot   0.004646353488232777
CDvis   0.0
CLff    0.3009503023520502
CYff    -7.714522820740938e-15
CDind   0.004646353488232777
CDff    0.004968969500908224
e       0.9669902146157929
StripForces 
Wing  cl =  [0.02994790451347, 0.08555545178934, 0.1329003532588, 0.1733025192695, 0.2100182422833, 0.2453427152547, 0.2792746996365, 0.310122128419, 0.3355632628223, 0.3531618776075, 0.3603457261533, 0.3542128805665, 0.3542128805661, 0.3603457261533, 0.3531618776088, 0.3355632628252, 0.3101221284236, 0.2792746996428, 0.2453427152623, 0.2100182422922, 0.1733025192801, 0.1329003532723, 0.08555545180788, 0.0299479045408]
Wing  cd =  [-0.004234137763162, -0.004494543653191, -0.003752887372724, -0.002739626801633, -0.001762021024326, -0.0007386538946403, 0.0005114598078396, 0.0021191472861, 0.004145189908974, 0.006609094404182, 0.009540018987595, 0.01315518814708, 0.01315518814718, 0.009540018987792, 0.00660909440444, 0.004145189909261, 0.002119147286385, 0.0005114598080998, -0.0007386538944071, -0.001762021024095, -0.002739626801367, -0.003752887372445, -0.004494543653161, -0.004234137764545]
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!

real	0m9.361s
user	0m0.030s
sys	0m0.062s
+ status=0
+ set +x

=================================================
Legacy CAPS verification (using pyCAPS) case avl_PyTest.py passed (as expected)
=================================================


=================================================
+ rm -rf avl_AutoSpan_PyTest
+ echo 'avl_AutoSpan_PyTest.py test;'
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
avl_AutoSpan_PyTest.py test;
+ python -u avl_AutoSpan_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Loading AIM
ERROR:: (name_not_found) in Branch Brch_000083 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\legacy\examples\csmData\avlWing.udc:114]]
        storage "Wing1Hinge" 1 not found
    --> catching signal -251 (name_not_found)
ERROR:: (name_not_found) in Branch Brch_000097 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\legacy\examples\csmData\avlWing.udc:138]]
        storage "Wing1Hinge" 1 not found
    --> catching signal -251 (name_not_found)
ERROR:: (name_not_found) in Branch Brch_000209 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\legacy\examples\csmData\avlWing.udc:114]]
        storage "Wing2Hinge" 1 not found
    --> catching signal -251 (name_not_found)
ERROR:: (name_not_found) in Branch Brch_000223 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\legacy\examples\csmData\avlWing.udc:138]]
        storage "Wing2Hinge" 1 not found
    --> catching signal -251 (name_not_found)
ERROR:: (name_not_found) in Branch Brch_000349 at [[C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\legacy\examples\csmData\avlWing.udc:138]]
        storage "Wing3Hinge" 3 not found
    --> catching signal -251 (name_not_found)
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 3
	Name = Wing1, index = 1
	Name = Wing2, index = 2
	Name = Wing3, index = 3
Getting vortex lattice surface data
	VLM surface name - Wing1
	VLM surface name - Wing2
	VLM surface name - Wing3
	Done getting vortex lattice surface data
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Warning: Control WingHinge1 not found in controls tuple! Only defaults will be used.
Writing surface - Wing1 (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing surface - Wing2 (ID = 1)
	Section 1 of 7 (ID = 0)
	Section 2 of 7 (ID = 1)
	Section 3 of 7 (ID = 2)
	Section 4 of 7 (ID = 3)
	Section 5 of 7 (ID = 4)
	Section 6 of 7 (ID = 5)
	Section 7 of 7 (ID = 6)
Writing surface - Wing3 (ID = 2)
	Section 1 of 7 (ID = 0)
	Section 2 of 7 (ID = 3)
	  Control surface 1 of 1 
	Section 3 of 7 (ID = 4)
	  Control surface 1 of 1 
	Section 4 of 7 (ID = 1)
	Section 5 of 7 (ID = 5)
	  Control surface 1 of 1 
	Section 6 of 7 (ID = 6)
	  Control surface 1 of 1 
	Section 7 of 7 (ID = 2)
Running AVL
CXtot   -0.03128890105581925
CYtot   -2.11044817062647e-11
CZtot   -1.014663137451587
Cltot   -6.716953065600433e-11
Cmtot   -2.941985138524829
Cntot   8.039869469200626e-12
Cl'tot  -6.70189853414633e-11
Cn'tot  9.210914907348648e-12
CLtot   1.01396253272292
CDtot   0.04899244907637161
CDvis   0.0
CLff    1.012753587462351
CYff    -2.520318523514418e-11
CDind   0.04899244907637161
CDff    -0.08941639978598759
e       -0.6085401584755901
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!

real	0m16.191s
user	0m0.030s
sys	0m0.062s
+ status=0
+ set +x

=================================================
Legacy CAPS verification (using pyCAPS) case avl_AutoSpan_PyTest.py passed (as expected)
=================================================


=================================================
+ rm -rf avl_DesignSweep_PyTest
+ echo 'avl_DesignSweep_PyTest.py test;'
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
avl_DesignSweep_PyTest.py test;
+ python -u avl_DesignSweep_PyTest.py -verbosity=0 -workDir=runDirectory -noPlotData
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
 Running AVL (sweep angle = 5) at Mach number = 0.05!
Cd = 0.002572533601559653
Cl = 0.2009337808878334
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
 Running AVL (sweep angle = 5) at Mach number = 0.1!
Cd = 0.002586364230250734
Cl = 0.2015191856819673
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control Tail not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightLE not found in controls tuple! Only defaults will be used.
Warning: Control WingRightTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
 Running AVL (sweep angle = 5) at Mach number = 0.15000000000000002!
The system cannot execute the specified program.
Traceback (most recent call last):
  File "C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\legacy\examples\pyCAPS\avl_DesignSweep_PyTest.py", line 81, in <module>
    myProblem.analysis[analysisID].postAnalysis()
  File "C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\pyCAPS\pyCAPS\problem.py", line 2159, in postAnalysis
    self._analysisObj.postAnalysis()
  File "C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\pyCAPS\pyCAPS\caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\pyCAPS\pyCAPS\caps.py", line 2913, in postAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\pyCAPS\pyCAPS\caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
avlAIM.c:2952 in aimPostAnalysis():
  Error: avl execution did not produce capsTotalForce.txt
================================================================================

WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!

real	0m14.006s
user	0m0.030s
sys	0m0.045s
+ status=1
+ set +x

=================================================
Legacy CAPS verification (using pyCAPS) case avl_DesignSweep_PyTest.py failed (as NOT expected)
=================================================


=================================================
+ rm -rf avl_ControlSurf_PyTest
+ echo 'avl_ControlSurf_PyTest.py test;'
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
avl_ControlSurf_PyTest.py test;
+ python -u avl_ControlSurf_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting design parameters
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 2
	Name = Wing, index = 1
	Name = Vertical_Tail, index = 2
Getting vortex lattice control surface data
	VLM control surface name - Tail
	VLM control surface name - WingRightLE
	VLM control surface name - WingRightTE
	Done getting vortex lattice control surface data
Getting vortex lattice surface data
	VLM surface name - Vertical_Tail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	Done getting vortex lattice surface data
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftLE not found in controls tuple! Only defaults will be used.
Warning: Control WingLeftTE not found in controls tuple! Only defaults will be used.
Writing surface - Vertical_Tail (ID = 0)
	Section 1 of 2 (ID = 0)
	  Control surface 1 of 1 
	Section 2 of 2 (ID = 1)
	  Control surface 1 of 1 
Writing surface - Wing (ID = 1)
	Section 1 of 3 (ID = 1)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
	Section 2 of 3 (ID = 0)
	  Control surface 1 of 4 
	  Control surface 2 of 4 
	  Control surface 3 of 4 
	  Control surface 4 of 4 
	Section 3 of 3 (ID = 2)
	  Control surface 1 of 2 
	  Control surface 2 of 2 
Running AVL
The system cannot execute the specified program.
Traceback (most recent call last):
  File "C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\legacy\examples\pyCAPS\avl_ControlSurf_PyTest.py", line 89, in <module>
    myAnalysis.postAnalysis()
  File "C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\pyCAPS\pyCAPS\problem.py", line 2159, in postAnalysis
    self._analysisObj.postAnalysis()
  File "C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\pyCAPS\pyCAPS\caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\pyCAPS\pyCAPS\caps.py", line 2913, in postAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\pyCAPS\pyCAPS\caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
avlAIM.c:2952 in aimPostAnalysis():
  Error: avl execution did not produce capsTotalForce.txt
================================================================================

WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!

real	0m6.893s
user	0m0.015s
sys	0m0.107s
+ status=1
+ set +x

=================================================
Legacy CAPS verification (using pyCAPS) case avl_ControlSurf_PyTest.py failed (as NOT expected)
=================================================


=================================================
+ rm -rf avl_EigenValue_PyTest
+ echo 'avl_EigenValue_PyTest.py test;'
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
avl_EigenValue_PyTest.py test;
+ python -u avl_EigenValue_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 1
	Name = Wing, index = 1
Getting vortex lattice surface data
	VLM surface name - Wing
	Done getting vortex lattice surface data
Writing surface - Wing (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing mass properties file: caps.mass
Parsing MassProp
Running AVL
Note: The following floating-point exceptions are signalling: IEEE_DIVIDE_BY_ZERO
EigenValues  ('case 1', [[0.48252996, 1.0092579], [0.48252996, -1.0092579], [-6.42569, 0.0], [-1.2733929, 0.0], [-0.0011487329, 0.0], [-1.2380479, 0.49321593], [-1.2380479, -0.49321593], [0.77888703, 0.0]])
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!

real	0m6.041s
user	0m0.031s
sys	0m0.061s
+ status=0
+ set +x

=================================================
Legacy CAPS verification (using pyCAPS) case avl_EigenValue_PyTest.py passed (as expected)
=================================================


=================================================
+ rm -rf awave_PyTest
+ echo 'awave_PyTest.py test;'
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
awave_PyTest.py test;
+ python -u awave_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Writing Awave input file
Body Section, Body ID 1
	XCG:   1.571025 -3.872983 0.270825
	AREA:  0.029452
	RAD:   0.096825
	ATTRIB:Store
	NAME  :RightWingTank
	Awave TYPE: 3

Body Section, Body ID 2
	XCG:   2.539271 -3.872983 0.270825
	AREA:  0.029452
	RAD:   0.096825
	ATTRIB:Store
	NAME  :RightWingTank
	Awave TYPE: 3

Body Section, Body ID 3
	XCG:   1.571025 3.872983 0.270825
	AREA:  0.029452
	RAD:   0.096825
	ATTRIB:Store
	NAME  :LeftWingTank
	Awave TYPE: 3

Body Section, Body ID 4
	XCG:   2.539271 3.872983 0.270825
	AREA:  0.029452
	RAD:   0.096825
	ATTRIB:Store
	NAME  :LeftWingTank
	Awave TYPE: 3

Lifting Surface Section, Body ID 5
	XLE:   1.571946 -3.872983 0.249728
	CHORD: 0.968408
	ATTRIB:Wing
	NAME  :Wing
	Awave TYPE: 0

Lifting Surface Section, Body ID 6
	XLE:   0.000000 0.000000 0.000000
	CHORD: 1.614013
	ATTRIB:Wing
	NAME  :Wing
	Awave TYPE: 1

Lifting Surface Section, Body ID 7
	XLE:   1.571946 3.872983 0.249728
	CHORD: 0.968408
	ATTRIB:Wing
	NAME  :Wing
	Awave TYPE: 1

Lifting Surface Section, Body ID 8
	XLE:   5.484123 0.000000 1.468246
	CHORD: 0.726185
	ATTRIB:VTail
	NAME  :VertTail
	Awave TYPE: 4

Lifting Surface Section, Body ID 9
	XLE:   5.000000 0.000000 0.500000
	CHORD: 1.210308
	ATTRIB:VTail
	NAME  :VertTail
	Awave TYPE: 4

Lifting Surface Section, Body ID 10
	XLE:   5.484123 -0.968246 0.500000
	CHORD: 0.726185
	ATTRIB:HTail
	NAME  :Stab
	Awave TYPE: 0

Lifting Surface Section, Body ID 11
	XLE:   5.484123 0.000000 0.500000
	CHORD: 0.726185
	ATTRIB:HTail
	NAME  :Stab
	Awave TYPE: 5

Lifting Surface Section, Body ID 12
	XLE:   5.484123 0.968246 0.500000
	CHORD: 0.726185
	ATTRIB:HTail
	NAME  :Stab
	Awave TYPE: 5

Body Section, Body ID 13
	XCG:   -2.000000 0.000000 0.000000
	AREA:  0.000000
	RAD:   0.000000
	ATTRIB:Fuse
	NAME  :Fuselage
	Awave TYPE: 2

Body Section, Body ID 14
	XCG:   0.000000 -0.000000 -0.000000
	AREA:  0.818123
	RAD:   0.510310
	ATTRIB:Fuse
	NAME  :Fuselage
	Awave TYPE: 2

Warning: capsGroup not found on body 15!
Body Section, Body ID 15
	XCG:   1.613743 -0.000000 0.000000
	AREA:  0.327249
	RAD:   0.322749
	ATTRIB:Fuse
	NAME  :(null)
	Awave TYPE: 2

Body Section, Body ID 16
	XCG:   5.000000 -0.000000 0.500000
	AREA:  0.081812
	RAD:   0.161374
	ATTRIB:Fuse
	NAME  :Fuselage
	Awave TYPE: 2

Body Section, Body ID 17
	XCG:   6.210307 -0.000000 0.500000
	AREA:  0.000818
	RAD:   0.016137
	ATTRIB:Fuse
	NAME  :Fuselage
	Awave TYPE: 2

AwaveTypes: 2 5 4 2 2
Points for all four fuselage sections :: 5 0 0 0
Number of Mach-Alpha cases = 2
 Running AWAVE 
 Running Post Analysis
CdWave =  [1.133363, 0.2164137]
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!

real	0m3.683s
user	0m0.000s
sys	0m0.092s
+ status=0
+ set +x

=================================================
Legacy CAPS verification (using pyCAPS) case awave_PyTest.py passed (as expected)
=================================================


=================================================
+ rm -rf friction_PyTest
+ echo 'friction_PyTest.py test;'
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
friction_PyTest.py test;
+ python -u friction_PyTest.py -verbosity=0 -workDir=runDirectory
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Loading AIM
Setting Mach & Altitude Values
Lifting Surface: Body = 1, units m
	XLE:   1.571946 -3.872983 0.249728
	XTE:   2.536563 -3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 2, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.614012 0.000000 0.002015
	Chord: 1.614013
	Arc:   3.308635
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 3, units m
	XLE:   1.571946 3.872983 0.249728
	XTE:   2.536563 3.872983 0.335335
	Chord: 0.968408
	Arc:   1.985181
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 4, units m
	XLE:   5.484123 0.000000 1.468246
	XTE:   6.210307 0.000915 1.468246
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 5, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.210307 0.001525 0.500000
	Chord: 1.210308
	Arc:   2.471195
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 6, units m
	XLE:   5.484123 -0.968246 0.500000
	XTE:   6.210307 -0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 7, units m
	XLE:   5.484123 0.968246 0.500000
	XTE:   6.210307 0.968246 0.500915
	Chord: 0.726185
	Arc:   1.482717
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 8, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 9, units m
	Arc: 3.714180
	Diameter: 1.020621
	Type: Fuse
Body of Revolution: Body = 10, units m
	Arc: 2.771209
	Diameter: 0.645497
	Type: Fuse
Body of Revolution: Body = 11, units m
	Arc: 1.013945
	Diameter: 0.322749
	Type: Fuse
Body of Revolution: Body = 12, units m
	Arc: 0.101394
	Diameter: 0.032275
	Type: Fuse
Number of sections 4, number of revolution sections 1
Number of Mach-Altitude cases = 2
Total drag = [0.0132, 0.01226]
Form drag = [0.0033, 0.00307]
Friction drag = [0.0099, 0.00919]
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!

real	0m3.496s
user	0m0.000s
sys	0m0.062s
+ status=0
+ set +x

=================================================
Legacy CAPS verification (using pyCAPS) case friction_PyTest.py passed (as expected)
=================================================


=================================================
+ rm -rf xfoil_PyTest
+ echo 'xfoil_PyTest.py test;'
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
xfoil_PyTest.py test;
+ python -u xfoil_PyTest.py -verbosity=0 -workDir=runDirectory -noPlotData
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt


Running xFoil......
Note: The following floating-point exceptions are signalling: IEEE_INVALID_FLAG IEEE_OVERFLOW_FLAG IEEE_DENORMAL
Cl =  [1.05475230552407, 1.36488869373582, 1.56607214272039, 2.03059709342836, 1.97271083120867, 1.87307153171894, 1.7605047576027]
Cd =  [0.0131991208675621, 0.0166540240606034, 0.0200551482563102, 0.0458671341983872, 0.0754256009397174, 0.0994469174482356, 0.127479430988808]
Alpha =  [0.0, 3.0, 5.0, 11.0, 13.0, 14.0, 15.0]
Transition location =  [0.496044114353196, 0.461377732041153, 0.442376568201411, 0.3612516363932, 0.276104140852458, 0.214381239321316, 0.132988264747733]
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!
WARNING: 'capsProblem.closeCAPS' is deprecated. Please use 'close'!

real	0m8.085s
user	0m0.015s
sys	0m0.123s
+ status=0
+ set +x

=================================================
Legacy CAPS verification (using pyCAPS) case xfoil_PyTest.py passed (as expected)
=================================================


=================================================
+ rm -rf autoLink_Pytest
+ echo 'autoLink_Pytest.py test;'
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
autoLink_Pytest.py test;
+ python -u autoLink_Pytest.py -verbosity=0 -workDir=runDirectory -noPlotData
+ tee -a /c/Users/jenkins/workspace/ESP_RegCaps/7.7/CAPS/LINEARAERO/WIN64.2019/CAPS/legacy/examples/regressionTest/pyCAPSlog.txt
Linked Parameter Mach to analysis frictionAIM input Mach
Linked Parameter Mach to analysis awaveAIM input Mach
Linked Parameter Mach to analysis avlAIM input Mach
Linked Parameter Alpha to analysis awaveAIM input Alpha
Linked Parameter Alpha to analysis avlAIM input Alpha
Linked Parameter Altitude to analysis frictionAIM input Altitude
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Mapping capsGroup attributes ................
	Number of unique capsGroup attributes = 6
	Name = RightTank, index = 1
	Name = LeftTank, index = 2
	Name = Wing, index = 3
	Name = VertTail, index = 4
	Name = HorizTail, index = 5
	Name = Fuselage, index = 6
Getting vortex lattice surface data
	VLM surface name - HorizTail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - VertTail
	No "groupName" variable provided or no matches found, going to use tuple name
	VLM surface name - Wing
	No "groupName" variable provided or no matches found, going to use tuple name
	Done getting vortex lattice surface data
Warning (vlm_getSections): No capsGroup value found on body 15, body will not be used
Warning (vlm_getSections): No capsGroup value found on body 15, body will not be used
Warning (vlm_getSections): No capsGroup value found on body 15, body will not be used
Writing surface - HorizTail (ID = 0)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Writing surface - VertTail (ID = 1)
	Section 1 of 2 (ID = 0)
	Section 2 of 2 (ID = 1)
Writing surface - Wing (ID = 2)
	Section 1 of 3 (ID = 0)
	Section 2 of 3 (ID = 1)
	Section 3 of 3 (ID = 2)
Running avlAIM
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
Body of Revolution: Body = 1, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 2, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 3, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Body of Revolution: Body = 4, units m
	Arc: 0.526861
	Diameter: 0.167705
	Type: Store
Lifting Surface: Body = 5, units m
	XLE:   1.361345 -3.354102 0.216271
	XTE:   2.196728 -3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 6, units m
	XLE:   0.000000 0.000000 0.000000
	XTE:   1.397775 0.000000 0.001745
	Chord: 1.397776
	Arc:   2.865362
	T/C:   0.127839
	Type: Wing
Lifting Surface: Body = 7, units m
	XLE:   1.361345 3.354102 0.216271
	XTE:   2.196728 3.354102 0.290409
	Chord: 0.838666
	Arc:   1.719217
	T/C:   0.155975
	Type: Wing
Lifting Surface: Body = 8, units m
	XLE:   5.419263 0.000000 1.338525
	XTE:   6.048157 0.000792 1.338525
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 9, units m
	XLE:   5.000000 0.000000 0.500000
	XTE:   6.048157 0.001321 0.500000
	Chord: 1.048158
	Arc:   2.140118
	T/C:   0.120035
	Type: VTail
Lifting Surface: Body = 10, units m
	XLE:   5.419263 -0.838525 0.500000
	XTE:   6.048157 -0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 11, units m
	XLE:   5.419263 0.000000 0.500000
	XTE:   6.048157 0.000000 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Lifting Surface: Body = 12, units m
	XLE:   5.419263 0.838525 0.500000
	XTE:   6.048157 0.838525 0.500792
	Chord: 0.628895
	Arc:   1.284071
	T/C:   0.120035
	Type: HTail
Body of Revolution: Body = 13, units m
	Arc: 0.000000
	Diameter: 0.000000
	Type: Fuse
Body of Revolution: Body = 14, units m
	Arc: 3.216574
	Diameter: 0.883883
	Type: Fuse
Body of Revolution: Body = 15, units m
	Arc: 2.399938
	Diameter: 0.559017
	Type: Fuse
Body of Revolution: Body = 16, units m
	Arc: 0.878102
	Diameter: 0.279508
	Type: Fuse
Body of Revolution: Body = 17, units m
	Arc: 0.087810
	Diameter: 0.027951
	Type: Fuse
Number of sections 5, number of revolution sections 1
Number of Mach-Altitude cases = 1
Running frictionAIM
Running avlAIM
The system cannot execute the specified program.
Traceback (most recent call last):
  File "C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\legacy\examples\pyCAPS\autoLink_Pytest.py", line 164, in <module>
    runAnalysis(myProblem)
  File "C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\legacy\examples\pyCAPS\autoLink_Pytest.py", line 46, in runAnalysis
    myAnalysis.postAnalysis()
  File "C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\pyCAPS\pyCAPS\problem.py", line 2159, in postAnalysis
    self._analysisObj.postAnalysis()
  File "C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\pyCAPS\pyCAPS\caps.py", line 999, in wrapper_checkClosed
    return func(*args, **kwargs)
           ^^^^^^^^^^^^^^^^^^^^^
  File "C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\pyCAPS\pyCAPS\caps.py", line 2913, in postAnalysis
    if stat: _raiseStatus(stat, errors=capsErrs(nErr, errs))
             ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^
  File "C:\Users\jenkins\workspace\ESP_RegCaps\7.7\CAPS\LINEARAERO\WIN64.2019\CAPS\pyCAPS\pyCAPS\caps.py", line 822, in _raiseStatus
    raise CAPSError(status, msg=msg, errors=errors)
pyCAPS.caps.CAPSError: CAPS_EXECERR:
================================================================================
avlAIM.c:2952 in aimPostAnalysis():
  Error: avl execution did not produce capsTotalForce.txt
================================================================================

WARNING: 'capsProblem.loadCAPS' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsGeometry.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsProblem.setVerbosity' is deprecated. Please use 'Problem.setOutLevel'!
WARNING: 'capsProblem.loadAIM' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsAnalysis.__init__' is deprecated. Please use 'Problem.analysis.create'!
WARNING: 'capsProblem.__init__' is deprecated. Please use 'Problem.__init__'!
WARNING: 'capsAnalysis.addAttribute' is deprecated. Please use 'Analysis.attr.create'!
WARNING: 'capsProblem.createValue' is deprecated. Please use 'Problem.parameter.create'!
WARNING: '_capsValue.__init__' is deprecated. Please use 'Problem.parameter.create'!
WARNING: 'capsProblem.autoLinkValue' is deprecated. Please use 'Problem.autoLinkParameter'!
WARNING: 'capsGeometry.setGeometryVal' is deprecated. Please use 'Problem.geometry.despmtr["varname"].value'!
WARNING: 'capsAnalysis.getAttributeVal' is deprecated. Please use 'Analysis.geometry.attrList'!
WARNING: 'capsAnalysis.setAnalysisVal' is deprecated. Please use 'Analysis.input["varname"].value'!
WARNING: 'capsAnalysis.aimName' is deprecated. Please use 'name'!
WARNING: 'capsAnalysis.getAttribute' is deprecated. Please use 'Analysis.attr["name"].value'!
WARNING: 'capsAnalysis.getAnalysisOutVal' is deprecated. Please use 'Analysis.output["varname"].value'!

real	0m25.823s
user	0m0.077s
sys	0m0.123s
+ status=1
+ set +x

=================================================
Legacy CAPS verification (using pyCAPS) case autoLink_Pytest.py failed (as NOT expected)
=================================================


*************************************************
*************************************************

=================================================
Legacy Did not run examples for:

tsfoil
=================================================
=================================================
Legacy Summary of examples NOT finished as expected

avl_DesignSweep_PyTest.py
avl_ControlSurf_PyTest.py
autoLink_Pytest.py

See pyCAPSlog.txt for more details.
=================================================
Build step 'Conditional step (single)' marked build as failure
[GNU C Compiler (gcc)Clang] Skipping execution of recorder since overall result is 'FAILURE'
[PostBuildScript] - [INFO] Executing post build scripts.
[PostBuildScript] - [INFO] build step #0 should only be executed on MATRIX
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Skipped based on build state FAILURE
Finished: FAILURE