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Passed

gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20210212155058)

Took 16 sec.

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 0.62 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 4.009e+10.

GP Solve 3
Using solver 'mosek_cli'
 
...[truncated 7477 chars]...
iff: [-97.19569911] dimensionless


Fuselage Cd Percent Diff: [108.78752887]


VT Cd Percent Diff: [-35.47578166] dimensionless


Wing Cd percent Diff: [-29.70474017]
Induced Drag Cd Percent Diff: [-33.71069184]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-5.63054334]




FUSELAGE DIFFERENCES




Weight of HB material: -48.577977708677565 


Weight of VB material: 117.29206246886021 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.80257498]
	

Standard Error

/jenkins/workspace/CE_gpkit_PR_research_models/buildnode/reynolds/optimizer/mosek/gpkit/constraints/gp.py:397: RuntimeWarning: divide by zero encountered in log
  for i, mi in enumerate(self.m_idxs) if la[i])