Passed

gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_conif (from gpkit.tests.from_paths.TestFiles-20210503171654)

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 0.36 seconds.
Solved cost was 3.965e+40.

GP Solve 2
Using solver 'mosek_cli'
 for 1198 free variables
  in 4699 posynomial inequalities.
Solving took 0.27 seconds.
Solved cost was 4.011e+10.

GP Solve 3
Using solver 'mosek_cli'
 
...[truncated 7512 chars]...
.19566057067883] dimensionless


Fuselage Cd Percent Diff: [108.78752887]


VT Cd Percent Diff: [-35.46214996502801] dimensionless


Wing Cd percent Diff: [-29.70220323]
Induced Drag Cd Percent Diff: [-33.70540902]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-5.63168751]




FUSELAGE DIFFERENCES




Weight of HB material: -48.5597697983582 


Weight of VB material: 117.2559386231767 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.80268981]
	

Standard Error

/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/constraints/gp.py:426: RuntimeWarning: divide by zero encountered in log
  for i, mi in enumerate(self.m_idxs) if la[i])