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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-20180605094909)

Took 0.97 sec.

Standard Output

Using solver 'cvxopt'
Solving for 11 variables.
Solving took 0.00772 seconds.
Using solver 'cvxopt'
Solving for 9 variables.
Solving took 0.00939 seconds.
Using solver 'cvxopt'
Solving for 25 variables.
Solving took 0.0254 seconds.
Using solver 'cvxopt'
Solving for 25 variables.
Solving took 0.0252 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 8.56 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 985.520045233 meter * revolutions_per_minute but the right hand side evaluated to 103.03888118 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 2.891832910281148 but the right hand side evaluated to 2.891823804935309 (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 0.420548336422 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420533437898 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 0.314622468452 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314607263016 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 0.16892681714 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168921962219 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 0.0639617339659 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639605304203 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 0.0226346738608 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226344198087 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%)

Using solver 'cvxopt'
Solving for 13 variables.
Solving took 0.0128 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 5.05 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 50.2429804544 meter / second but the right hand side evaluated to 50.2427628677 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 2.9030232085212324 but the right hand side evaluated to 2.902960628166081 (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 1619892.1265 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 4.26126804921 meter ** 2 / second ** 2 but the right hand side evaluated to 4.26105171174 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 1849726.5700 but bound is 1000000.0000
Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1849726.5566 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 1928321.4295 but bound is 700000.0000

Standard Error