Passed

gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20210824195841)

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 0.529 seconds.
Solved cost was 3.965e+40.

GP Solve 2
Using solver 'mosek_cli'
 for 1198 free variables
  in 4699 posynomial inequalities.
Solving took 0.399 seconds.
Solved cost was 4.006e+10.

GP Solve 3
Using solver 'mosek_cli'

...[truncated 7509 chars]...
565967702238] dimensionless


Fuselage Cd Percent Diff: [108.78752887]


VT Cd Percent Diff: [-35.461857717429076] dimensionless


Wing Cd percent Diff: [-29.70224786]
Induced Drag Cd Percent Diff: [-33.70551751]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-5.63190011]




FUSELAGE DIFFERENCES




Weight of HB material: -48.558425165327215 


Weight of VB material: 117.25661657216746 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.80269126]

Standard Error

/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]))