Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20180111113112)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -2.484698644750205e-13. Allowing negative dual variable(s) as small as -5.06138100181408e-13. Allowing negative dual variable(s) as small as -9.730302501231858e-14. Allowing negative dual variable(s) as small as -8.253987771045246e-14. Solving took 4 GP solves and 4.03 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -2.614549202140104e-13. Allowing negative dual variable(s) as small as -4.661065370475947e-13. Allowing negative dual variable(s) as small as -5.897712873625949e-14. Allowing negative dual variable(s) as small as -4.8133589128362964e-14. Solving took 4 GP solves and 3.7 seconds. MTOW [lbs] = 132.52 Zero fuel weight [lbs] = 53.63 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 20.351 speed at top of climb [m/s] = 25.000 design loiter speed [m/s] = 25.000 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 27.299 optimum loiter speed for min power, start of loiter [m/s] = 23.617 optimum loiter speed for min power, end of loiter [m/s] = 16.684 optimum cruise speed, inbound [m/s] = 31.019 optimum cruise speed, outbound [m/s] = 23.408 Beginning signomial solve. Allowing negative dual variable(s) as small as -5.027451018135615e-12. Allowing negative dual variable(s) as small as -1.1071713533049294e-12. Allowing negative dual variable(s) as small as -2.483333462206146e-12. Allowing negative dual variable(s) as small as -2.4820090671473076e-12. Solving took 4 GP solves and 3.25 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 2.36 seconds. Max payload weight [lbf] = 9.202 Max take off weight [lbf] = 140.328 MTOW [lbs] = 132.52 Zero fuel weight [lbs] = 53.63 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 20.351 speed at top of climb [m/s] = 25.000 design loiter speed [m/s] = 25.000 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 27.299 optimum loiter speed for min power, start of loiter [m/s] = 23.617 optimum loiter speed for min power, end of loiter [m/s] = 16.684 optimum cruise speed, inbound [m/s] = 31.019 optimum cruise speed, outbound [m/s] = 23.408 Beginning signomial solve. Allowing negative dual variable(s) as small as -5.027281249942505e-12. Allowing negative dual variable(s) as small as -1.1070833023722147e-12. Allowing negative dual variable(s) as small as -2.483295105056975e-12. Allowing negative dual variable(s) as small as -2.4820131681532747e-12. Solving took 4 GP solves and 3.58 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 2.22 seconds. Max payload weight [lbf] = 9.202 Max take off weight [lbf] = 140.328