Passed
gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20210624151559)
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 1.65 seconds. Solved cost was 3.965e+40. GP Solve 2 Using solver 'mosek_cli' for 1198 free variables in 4699 posynomial inequalities. Solving took 0.979 seconds. Solved cost was 4.013e+10. GP Solve 3 Using solver 'mosek_cli' ...[truncated 4575 chars]... Diff: [-97.20244273] dimensionless Fuselage Cd Percent Diff: [108.78744865] VT Cd Percent Diff: [-35.6733968] dimensionless Wing Cd percent Diff: [-29.62869661] Induced Drag Cd Percent Diff: [-33.69778717] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-5.54291212] FUSELAGE DIFFERENCES Weight of HB material: -30.556822010234267 Weight of VB material: 115.861952322752 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.80046743]