Passed

gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20210212155403)

Standard Output

Starting a sequence of GP solves
 for 317 free variables
  in 136 locally-GP constraints
  and for 1198 free variables
       in 4699 posynomial inequalities.

GP Solve 1
Using solver 'mosek_cli'
 for 1198 free variables
  in 4699 posynomial inequalities.
Solving took 1.04 seconds.
Solved cost was 3.965e+40.

GP Solve 2
Using solver 'mosek_cli'
 for 1198 free variables
  in 4699 posynomial inequalities.
Solving took 0.754 seconds.
Solved cost was 4.017e+10.

GP Solve 3
Using solver 'mosek_cli'

...[truncated 4640 chars]...
iff: [-97.20240636] dimensionless


Fuselage Cd Percent Diff: [108.78744865]


VT Cd Percent Diff: [-35.67288219] dimensionless


Wing Cd percent Diff: [-29.62862624]
Induced Drag Cd Percent Diff: [-33.69745566]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-5.5432994]




FUSELAGE DIFFERENCES




Weight of HB material: -30.620819113142822 


Weight of VB material: 115.89562941405917 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.80047319]