Passed
gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20211026162557)
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 0.554 seconds. Solved cost was 3.965e+40. GP Solve 2 Using solver 'mosek_cli' for 1198 free variables in 4699 posynomial inequalities. Solving took 0.369 seconds. Solved cost was 4.012e+10. GP Solve 3 Using solver 'mosek_cli' ...[truncated 4604 chars]... 97.20243713311] dimensionless Fuselage Cd Percent Diff: [108.78744865] VT Cd Percent Diff: [-35.673075170471975] dimensionless Wing Cd percent Diff: [-29.62876698] Induced Drag Cd Percent Diff: [-33.69798608] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-5.54327106] FUSELAGE DIFFERENCES Weight of HB material: -30.6061785614518 Weight of VB material: 115.86303163521194 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.80047271]