Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.166353456154127e-14.
Allowing negative dual variable(s) as small as -7.574409849331332e-14.
Allowing negative dual variable(s) as small as -1.5050807822269974e-13.
Allowing negative dual variable(s) as small as -1.4987143470701625e-13.
Solving took 4 GP solves and 1.77 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.088117427387573e-14.
Allowing negative dual variable(s) as small as -7.116226011238957e-14.
Allowing negative dual variable(s) as small as -1.5118852350615164e-13.
Allowing negative dual variable(s) as small as -1.4889998956046924e-13.
Solving took 4 GP solves and 4.97 seconds.
Allowing negative dual variable(s) as small as -5.175183198646849e-13.
Allowing negative dual variable(s) as small as -1.430307261518493e-12.
Allowing negative dual variable(s) as small as -4.4415512934214973e-13.
Allowing negative dual variable(s) as small as -4.4472932281269806e-13.
Allowing negative dual variable(s) as small as -1.2962127031446169e-12.
Allowing negative dual variable(s) as small as -1.0903269389780923e-12.
Allowing negative dual variable(s) as small as -1.0901917389671834e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
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 = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.484857738713523e-14.
Allowing negative dual variable(s) as small as -5.6960910089149285e-12.
Allowing negative dual variable(s) as small as -2.0879030357589822e-11.
Allowing negative dual variable(s) as small as -2.088067140184234e-11.
Solving took 4 GP solves and 2.93 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.36 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.176241379967195e-13.
Allowing negative dual variable(s) as small as -1.4304130796505277e-12.
Allowing negative dual variable(s) as small as -4.4616567385080685e-13.
Allowing negative dual variable(s) as small as -4.4499993967495044e-13.
Allowing negative dual variable(s) as small as -1.2959613850810348e-12.
Allowing negative dual variable(s) as small as -1.0897119795058585e-12.
Allowing negative dual variable(s) as small as -1.0918259569017708e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
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 = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -5.273559366969494e-16.
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.4589411880934135e-14.
Allowing negative dual variable(s) as small as -5.6958897812034735e-12.
Allowing negative dual variable(s) as small as -2.087904167614699e-11.
Allowing negative dual variable(s) as small as -2.088082447858948e-11.
Solving took 4 GP solves and 1.66 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.5 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Passed

Standard Output

Standard Error
