Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.085255133652211e-14.
Allowing negative dual variable(s) as small as -7.420973557881183e-14.
Allowing negative dual variable(s) as small as -1.5152462617962215e-13.
Allowing negative dual variable(s) as small as -1.4805344450419256e-13.
Solving took 4 GP solves and 3.47 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.166396824241026e-14.
Allowing negative dual variable(s) as small as -7.532993326342385e-14.
Allowing negative dual variable(s) as small as -1.522454037838905e-13.
Allowing negative dual variable(s) as small as -1.4957219490741025e-13.
Solving took 4 GP solves and 3.41 seconds.
Allowing negative dual variable(s) as small as -5.179953688205785e-13.
Allowing negative dual variable(s) as small as -1.4293167344137103e-12.
Allowing negative dual variable(s) as small as -4.445385032303406e-13.
Allowing negative dual variable(s) as small as -4.450780022313694e-13.
Allowing negative dual variable(s) as small as -1.2971360097147056e-12.
Allowing negative dual variable(s) as small as -1.0914506061096563e-12.
Allowing negative dual variable(s) as small as -1.0903196748235366e-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 -2.4830771589913643e-14.
Allowing negative dual variable(s) as small as -5.696017586722632e-12.
Allowing negative dual variable(s) as small as -2.087898621023261e-11.
Allowing negative dual variable(s) as small as -2.088089343742107e-11.
Solving took 4 GP solves and 3.36 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.34 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.18710074892681e-13.
Allowing negative dual variable(s) as small as -1.429713986089709e-12.
Allowing negative dual variable(s) as small as -4.443077850080357e-13.
Allowing negative dual variable(s) as small as -4.434005246300998e-13.
Allowing negative dual variable(s) as small as -1.2981976604820034e-12.
Allowing negative dual variable(s) as small as -1.0898211586646278e-12.
Allowing negative dual variable(s) as small as -1.0895535775684584e-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 -2.0027382530152238e-15.
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 -2.4358659459673975e-14.
Allowing negative dual variable(s) as small as -5.69604305530929e-12.
Allowing negative dual variable(s) as small as -2.0878951690357758e-11.
Allowing negative dual variable(s) as small as -2.0880936771679592e-11.
Solving took 4 GP solves and 3.46 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 3.3 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Passed

Standard Output

Standard Error
