Passed

gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_conif (from gpkit.tests.from_paths.TestFiles-20200714165704)

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 0.369 seconds.
Solved cost was 3.965e+40.

GP Solve 2
Using solver 'mosek_cli'
 for 1198 free variables
  in 4705 posynomial inequalities.
Solving took 0.297 seconds.
Solved cost was 4.016e+10.

GP Solve 3
Using solver 'mosek_cli'
...[truncated 8470 chars]...
.1958590570307] dimensionless


Fuselage Cd Percent Diff: [108.78752887]


VT Cd Percent Diff: [-35.47396486505523] dimensionless


Wing Cd percent Diff: [-29.70482259]
Induced Drag Cd Percent Diff: [-33.71230076]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-5.63054768]




FUSELAGE DIFFERENCES




Weight of HB material: -48.57322592540589 


Weight of VB material: 117.1900315191087 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.80258386]
	

Standard Error

/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/constraints/gp.py:407: RuntimeWarning: divide by zero encountered in log
  for i, mi in enumerate(self.m_idxs) if la[i])