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Passed

gpkit.tests.from_paths.TestFiles.test_gpkitmodels_GP_aircraft_tail_tail_tests_py_cvxopt (from gpkit.tests.from_paths.TestFiles-20180424135342)

Took 2.2 sec.

Standard Output

Using solver 'cvxopt'
Solving for 11 variables.
Solving took 0.00858 seconds.
Using solver 'cvxopt'
Solving for 9 variables.
Solving took 0.00881 seconds.
Using solver 'cvxopt'
Solving for 25 variables.
Solving took 0.0255 seconds.
Using solver 'cvxopt'
Solving for 25 variables.
Solving took 0.0252 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 18.5 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 985.520044963 meter * revolutions_per_minute but the right hand side evaluated to 103.038881157 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 2.891832909507874 but the right hand side evaluated to 2.8918238041651403 (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 0.420548336038 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420533437516 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 0.314622468202 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314607262768 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 0.168926817034 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168921962113 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 0.0639617342893 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639605307439 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 0.02263467385 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226344197979 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%)

Using solver 'cvxopt'
Solving for 13 variables.
Solving took 0.0107 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 12.6 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 50.2429804541 meter / second but the right hand side evaluated to 50.2427628674 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 2.9030232087051937 but the right hand side evaluated to 2.902960628376678 (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 1619892.1243 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 4.26126804067 meter ** 2 / second ** 2 but the right hand side evaluated to 4.2610517033 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 1849726.5738 but bound is 1000000.0000
Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1849726.5544 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