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gpkit.tests.from_paths.TestFiles.test_gpkitmodels_GP_aircraft_fuselage_test_fuselage_py_cvxopt (from gpkit.tests.from_paths.TestFiles-20180605125443)

Took 0.75 sec.

Standard Output

Using solver 'cvxopt'
Solving for 11 variables.
Solving took 0.028 seconds.
Using solver 'cvxopt'
Solving for 9 variables.
Solving took 0.017 seconds.
Using solver 'cvxopt'
Solving for 25 variables.
Solving took 0.068 seconds.
Using solver 'cvxopt'
Solving for 25 variables.
Solving took 0.054 seconds.
Beginning signomial solve.
Solving took 16 GP solves and 13.7 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 985.52004502 meter * revolutions_per_minute but the right hand side evaluated to 103.038881161 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 2.891832909670814 but the right hand side evaluated to 2.891823804321586 (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 0.420548336117 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420533437593 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 0.314622468254 meter ** 2 / second ** 2 but the right hand side evaluated to 0.31460726282 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 0.168926817056 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168921962135 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 0.0639617342227 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639605306772 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 0.0226346738522 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226344198002 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%)

Using solver 'cvxopt'
Solving for 13 variables.
Solving took 0.021 seconds.
Beginning signomial solve.
Solving took 11 GP solves and 11.2 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 50.2427628675 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 2.903023208624635 but the right hand side evaluated to 2.9029606282844953 (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 1619892.1252 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 4.26126804441 meter ** 2 / second ** 2 but the right hand side evaluated to 4.261051707 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