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Passed

gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20201203200411)

Took 1 min 0 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 2.59 seconds.
Solved cost was 3.965e+40.

GP Solve 2
Using solver 'mosek_cli'
 for 1198 free variables
  in 4699 posynomial inequalities.
Solving took 0.791 seconds.
Solved cost was 4.011e+10.

GP Solve 3
Using solver 'mosek_cli'

...[truncated 7463 chars]...
 Diff: [-97.19579658] dimensionless


Fuselage Cd Percent Diff: [108.78752887]


VT Cd Percent Diff: [-35.47039296] dimensionless


Wing Cd percent Diff: [-29.70421106]
Induced Drag Cd Percent Diff: [-33.71057445]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-5.6310938]




FUSELAGE DIFFERENCES




Weight of HB material: -48.56918788778248 


Weight of VB material: 117.21428542948884 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.80261287]
	

Standard Error

/jenkins/workspace/CE_gpkit_PR_research_models/buildnode/reynolds/optimizer/mosek/gpkit/constraints/gp.py:390: RuntimeWarning: divide by zero encountered in log
  for i, mi in enumerate(self.m_idxs) if la[i])