Passed

gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20210816211509)

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 0.357 seconds.
Solved cost was 3.965e+40.

GP Solve 2
Using solver 'mosek_cli'
 for 1198 free variables
  in 4699 posynomial inequalities.
Solving took 0.261 seconds.
Solved cost was 4.01e+10.

GP Solve 3
Using solver 'mosek_cli'
 
...[truncated 7513 chars]...
19565948384317] dimensionless


Fuselage Cd Percent Diff: [108.78752887]


VT Cd Percent Diff: [-35.46174811790299] dimensionless


Wing Cd percent Diff: [-29.70222418]
Induced Drag Cd Percent Diff: [-33.70550546]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-5.63180444]




FUSELAGE DIFFERENCES




Weight of HB material: -48.55992306376447 


Weight of VB material: 117.25608603838137 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.80269278]

Standard Error

/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/constraints/gp.py:430: RuntimeWarning: divide by zero encountered in log
  b[mi] - np.log(self.nu_by_posy[i]/la[i]))