Passed

gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20200715180043)

Standard Output

Starting a sequence of GP solves
 for 317 free variables
  in 136 locally-GP constraints
  and for 1198 free variables
       in 4705 posynomial inequalities.

GP Solve 1
Using solver 'mosek_cli'
 for 1198 free variables
  in 4705 posynomial inequalities.
Solving took 0.983 seconds.
Solved cost was 3.965e+40.

GP Solve 2
Using solver 'mosek_cli'
 for 1198 free variables
  in 4705 posynomial inequalities.
Solving took 0.739 seconds.
Solved cost was 4.007e+10.

GP Solve 3
Using solver 'mosek_cli'
...[truncated 5259 chars]...
ff: [-97.20242874] dimensionless


Fuselage Cd Percent Diff: [108.78744865]


VT Cd Percent Diff: [-35.67281786] dimensionless


Wing Cd percent Diff: [-29.62876698]
Induced Drag Cd Percent Diff: [-33.69785347]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-5.54357332]




FUSELAGE DIFFERENCES




Weight of HB material: -30.657719021128855 


Weight of VB material: 115.86648547134872 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.80047751]
		

Standard Error