Passed

gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20200416162330)

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 0.387 seconds.
Solved cost was 3.965e+40.

GP Solve 2
Using solver 'mosek_cli'
 for 1198 free variables
  in 4705 posynomial inequalities.
Solving took 0.331 seconds.
Solved cost was 4.01e+10.

GP Solve 3
Using solver 'mosek_cli'

...[truncated 8469 chars]...
1957682702787] dimensionless


Fuselage Cd Percent Diff: [108.78752887]


VT Cd Percent Diff: [-35.46689856667439] dimensionless


Wing Cd percent Diff: [-29.70338958]
Induced Drag Cd Percent Diff: [-33.70895417]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-5.63120633]




FUSELAGE DIFFERENCES




Weight of HB material: -48.56411390849966 


Weight of VB material: 117.22048168813754 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.80264357]
	

Standard Error

/Users/jenkins/workspace/CE_RM_SPaircraft_Push/mosek/gpkit/gpkit/constraints/gp.py:403: RuntimeWarning: divide by zero encountered in log
  for i, mi in enumerate(self.m_idxs) if la[i])