Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.895216176858952e-14.
Allowing negative dual variable(s) as small as -7.59626736512864e-14.
Allowing negative dual variable(s) as small as -1.5116770682443992e-13.
Allowing negative dual variable(s) as small as -1.488275648553472e-13.
Solving took 4 GP solves and 3.02 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.235742395193199e-14.
Allowing negative dual variable(s) as small as -7.533687215732776e-14.
Allowing negative dual variable(s) as small as -1.5113301235492038e-13.
Allowing negative dual variable(s) as small as -1.4954183724658066e-13.
Solving took 4 GP solves and 3.09 seconds.
Allowing negative dual variable(s) as small as -5.151989945773039e-13.
Allowing negative dual variable(s) as small as -1.4268117937143998e-12.
Allowing negative dual variable(s) as small as -4.436399164697846e-13.
Allowing negative dual variable(s) as small as -4.432912370511133e-13.
Allowing negative dual variable(s) as small as -1.297172438907701e-12.
Allowing negative dual variable(s) as small as -1.0913055398589777e-12.
Allowing negative dual variable(s) as small as -1.091214900557358e-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 -1.2555061157382141e-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 -2.4465827656347365e-14.
Allowing negative dual variable(s) as small as -5.695962676541277e-12.
Allowing negative dual variable(s) as small as -2.0879046328369573e-11.
Allowing negative dual variable(s) as small as -2.088077890808457e-11.
Solving took 4 GP solves and 3.08 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.96 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.169250444359008e-13.
Allowing negative dual variable(s) as small as -1.429184895429536e-12.
Allowing negative dual variable(s) as small as -4.437908374121946e-13.
Allowing negative dual variable(s) as small as -4.4295123124982183e-13.
Allowing negative dual variable(s) as small as -1.2969347817914922e-12.
Allowing negative dual variable(s) as small as -1.0901395888426868e-12.
Allowing negative dual variable(s) as small as -1.0907505367668824e-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 -2.477564086235482e-14.
Allowing negative dual variable(s) as small as -5.696072412835967e-12.
Allowing negative dual variable(s) as small as -2.0878930799560664e-11.
Allowing negative dual variable(s) as small as -2.0880808627638422e-11.
Solving took 4 GP solves and 2.9 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.35 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Passed

Standard Output

Standard Error
