Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.0964441000722616e-14.
Allowing negative dual variable(s) as small as -7.307002225509507e-14.
Allowing negative dual variable(s) as small as -1.4965372691078116e-13.
Allowing negative dual variable(s) as small as -1.4989485347394194e-13.
Solving took 4 GP solves and 1.71 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.0799208589635825e-14.
Allowing negative dual variable(s) as small as -7.570203144902088e-14.
Allowing negative dual variable(s) as small as -1.5119719712353152e-13.
Allowing negative dual variable(s) as small as -1.4940999826240642e-13.
Solving took 4 GP solves and 2.03 seconds.
Allowing negative dual variable(s) as small as -5.164531996504351e-13.
Allowing negative dual variable(s) as small as -1.4299689904406776e-12.
Allowing negative dual variable(s) as small as -4.4561229706197025e-13.
Allowing negative dual variable(s) as small as -4.429824562723894e-13.
Allowing negative dual variable(s) as small as -1.2979032995921735e-12.
Allowing negative dual variable(s) as small as -1.091828667407202e-12.
Allowing negative dual variable(s) as small as -1.0908848694160533e-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 -3.8077180297690916e-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 -2.490211082231377e-14.
Allowing negative dual variable(s) as small as -5.695999135751002e-12.
Allowing negative dual variable(s) as small as -2.087890496640573e-11.
Allowing negative dual variable(s) as small as -2.0880792395707826e-11.
Solving took 4 GP solves and 4.73 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.19 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.171679057225376e-13.
Allowing negative dual variable(s) as small as -1.4311728885330055e-12.
Allowing negative dual variable(s) as small as -4.4396777920674424e-13.
Allowing negative dual variable(s) as small as -4.45555051187263e-13.
Allowing negative dual variable(s) as small as -1.2969963644748894e-12.
Allowing negative dual variable(s) as small as -1.0911537515548297e-12.
Allowing negative dual variable(s) as small as -1.090691881429351e-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 -2.5357274140916234e-14.
Allowing negative dual variable(s) as small as -5.6960093788145544e-12.
Allowing negative dual variable(s) as small as -2.087895526793376e-11.
Allowing negative dual variable(s) as small as -2.0880742739327736e-11.
Solving took 4 GP solves and 2.15 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.9 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Passed

Standard Output

Standard Error
