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Passed

gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20200304030143)

Took 19 sec.

Standard Output

Starting a sequence of GP solves
 for 237 free variables
  in 136 signomial constraints
  and for 1196 free variables
       in 4701 posynomial inequalities.

GP Solve 1
Using solver 'mosek_cli'
 for 1196 free variables
  in 4701 posynomial inequalities.
Solving took 0.424 seconds.
Solved cost was 3.965e+40.

GP Solve 2
Using solver 'mosek_cli'
 for 1196 free variables
  in 4701 posynomial inequalities.
Solving took 0.421 seconds.
Solved cost was 4.014e+10.

GP Solve 3
Using solver 'mosek_cli'

...[truncated 5081 chars]...
43433554572] dimensionless


Fuselage Cd Percent Diff: [108.78744865]


VT Cd Percent Diff: [-35.673203824192996] dimensionless


Wing Cd percent Diff: [-29.62876698]
Induced Drag Cd Percent Diff: [-33.69798608]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-5.54332773]




FUSELAGE DIFFERENCES




Weight of HB material: -30.605692803001627 


Weight of VB material: 115.86778067414713 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.80047175]
	

Standard Error