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Passed

gpkit.tests.from_paths.TestFiles.test_gpkitmodels_GP_aircraft_motor_motor_test_py_cvxopt (from gpkit.tests.from_paths.TestFiles-20180430060803)

Took 10 sec.

Standard Output

Using solver 'cvxopt'
Solving for 11 variables.
Solving took 0.00792 seconds.
Using solver 'cvxopt'
Solving for 9 variables.
Solving took 0.0151 seconds.
Using solver 'cvxopt'
Solving for 25 variables.
Solving took 0.0423 seconds.
Using solver 'cvxopt'
Solving for 25 variables.
Solving took 0.0259 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 9.99 seconds.
Warning: Constraint [dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,) + dT_BladeElem... >= T_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp [lbf]...] is not tight because the left hand side evaluated to 100.006552841 force_pound but the right hand side evaluated to 100.0 force_pound (Allowable error: 0.0001%, Actual error: 0.0066%)

Warning: Constraint [omega_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)*r_BladeElem... >= Wt_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,) + vt_BladeElem...] is not tight because the left hand side evaluated to 985.520045025 meter * revolutions_per_minute but the right hand side evaluated to 103.038881162 meter / second (Allowable error: 0.0001%, Actual error: 0.16%)

Warning: Constraint [0.5*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)*lam_w_Blade... >= 1.64*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)*R_BladeEle...] is not tight because the left hand side evaluated to 2.8918329096854944 but the right hand side evaluated to 2.891823804338708 (Allowable error: 0.0001%, Actual error: 0.00031%)

Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.420548336125 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420533437602 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0035%)

Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.314622468259 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314607262825 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0048%)

Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.168926817058 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168921962137 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0029%)

Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.0639617342153 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639605306698 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0019%)

Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.0226346738525 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226344198004 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%)

Using solver 'cvxopt'
Solving for 13 variables.
Solving took 0.0196 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 5.81 seconds.
Warning: Constraint [Wa_BladeElementProp/BladeElementPerf_(0,) [m/s]... >= V_FlightState.1 + va_BladeElementProp/BladeElementPerf_(0,) [m/s]...] is not tight because the left hand side evaluated to 50.2429804543 meter / second but the right hand side evaluated to 50.2427628676 meter / second (Allowable error: 0.0001%, Actual error: 0.00043%)

Warning: Constraint [omega_BladeElementProp/BladeElementPerf_(0,)*r_BladeElementProp/BladeElementPerf_(0,) [m*rpm]... >= Wt_BladeElementProp/BladeElementPerf_(0,) + vt_BladeElementProp/BladeElementPerf_(0,) [m/s]...] is not tight because the left hand side evaluated to 147.268779253 meter * revolutions_per_minute but the right hand side evaluated to 15.4218953994 meter / second (Allowable error: 0.0001%, Actual error: 0.00036%)

Warning: Constraint [0.5*B_BladeElementProp/BladeElementPerf_(0,)*lam_w_BladeElementProp/BladeElementPerf_(0,)**-1... >= 1.64*B_BladeElementProp/BladeElementPerf_(0,)*R_Propeller.1**-1*lam_w_BladeElementProp/BladeElementP...] is not tight because the left hand side evaluated to 2.9030232086032126 but the right hand side evaluated to 2.9029606282605482 (Allowable error: 0.0001%, Actual error: 0.0022%)

Warning: Variable [cl_BladeElementProp/BladeElementPerf_(0,), cl_BladeElementProp/BladeElementPerf_(1,), cl_BladeEleme could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742
Warning: Variable [Re_BladeElementProp/BladeElementPerf_(0,), Re_BladeElementProp/BladeElementPerf_(1,), Re_BladeEleme could cause inaccurate result because it is above upper bound. Solution is 1619892.1255 but bound is 700000.0000
Warning: Constraint [0.151*B_BladeElementProp/BladeElementPerf_(0,)**-2*F_BladeElementProp/BladeElementPerf_(0,)**2*R_Pro... >= 0.00633*B_BladeElementProp/BladeElementPerf_(0,)**2*G_BladeElementProp/BladeElementPerf_(0,)**2*r_Bl...] is not tight because the left hand side evaluated to 4.26126804542 meter ** 2 / second ** 2 but the right hand side evaluated to 4.26105170799 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0051%)

Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220952.3405 but bound is 1000000.0000
Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.5667 but bound is 1000000.0000
Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2223840.1738 but bound is 1000000.0000
Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2223840.1106 but bound is 1000000.0000
Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1849726.5831 but bound is 1000000.0000
Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1849726.5819 but bound is 1000000.0000
Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 2197590.3832 but bound is 700000.0000
Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1681137.7135 but bound is 700000.0000

Standard Error