Passed
gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20220329165110)
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 0.687 seconds. Solved cost was 3.965e+40. GP Solve 2 Using solver 'mosek_cli' for 1198 free variables in 4699 posynomial inequalities. Solving took 0.49 seconds. Solved cost was 4.01e+10. GP Solve 3 Using solver 'mosek_cli' f ...[truncated 4608 chars]... 0242874040878] dimensionless Fuselage Cd Percent Diff: [108.78744865] VT Cd Percent Diff: [-35.67294651649368] dimensionless Wing Cd percent Diff: [-29.62869661] Induced Drag Cd Percent Diff: [-33.69778717] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-5.54334663] FUSELAGE DIFFERENCES Weight of HB material: -30.633861173157538 Weight of VB material: 115.86821241014019 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.80047415]