Passed

gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20200422083732)

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 1.03 seconds.
Solved cost was 3.965e+40.

GP Solve 2
Using solver 'mosek_cli'
 for 1198 free variables
  in 4705 posynomial inequalities.
Solving took 0.925 seconds.
Solved cost was 4.009e+10.

GP Solve 3
Using solver 'mosek_cli'

...[truncated 5254 chars]...
Diff: [-97.20243713] dimensionless


Fuselage Cd Percent Diff: [108.78744865]


VT Cd Percent Diff: [-35.67326815] dimensionless


Wing Cd percent Diff: [-29.62876698]
Induced Drag Cd Percent Diff: [-33.69805238]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-5.54309159]




FUSELAGE DIFFERENCES




Weight of HB material: -30.57188954497141 


Weight of VB material: 115.8649744112391 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.80046887]
		

Standard Error