Passed
gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20220329204746)
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 0.645 seconds. Solved cost was 3.965e+40. GP Solve 2 Using solver 'mosek_cli' for 1198 free variables in 4699 posynomial inequalities. Solving took 0.483 seconds. Solved cost was 4.007e+10. GP Solve 3 Using solver 'mosek_cli' ...[truncated 4611 chars]... 0243713310997] dimensionless Fuselage Cd Percent Diff: [108.78744865] VT Cd Percent Diff: [-35.67339680429208] dimensionless Wing Cd percent Diff: [-29.62876698] Induced Drag Cd Percent Diff: [-33.69798608] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-5.54287434] FUSELAGE DIFFERENCES Weight of HB material: -30.544043289877937 Weight of VB material: 115.86626960497115 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.80046599]