Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.080267803658778e-14.
Allowing negative dual variable(s) as small as -7.71518265940685e-14.
Allowing negative dual variable(s) as small as -1.5210792694841935e-13.
Allowing negative dual variable(s) as small as -1.4981158674709505e-13.
Solving took 4 GP solves and 4.49 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.1423709040987475e-14.
Allowing negative dual variable(s) as small as -7.687210243356724e-14.
Allowing negative dual variable(s) as small as -1.51310821511208e-13.
Allowing negative dual variable(s) as small as -1.4949933652141922e-13.
Solving took 4 GP solves and 5.55 seconds.
Allowing negative dual variable(s) as small as -5.168088179630104e-13.
Allowing negative dual variable(s) as small as -1.432036780824042e-12.
Allowing negative dual variable(s) as small as -4.431767453016988e-13.
Allowing negative dual variable(s) as small as -4.450866758487493e-13.
Allowing negative dual variable(s) as small as -1.2978605820265776e-12.
Allowing negative dual variable(s) as small as -1.0908599327660862e-12.
Allowing negative dual variable(s) as small as -1.0899060516947334e-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 -2.445910401469118e-14.
Allowing negative dual variable(s) as small as -5.696060652471709e-12.
Allowing negative dual variable(s) as small as -2.0879038473938932e-11.
Allowing negative dual variable(s) as small as -2.088076471228883e-11.
Solving took 4 GP solves and 14.3 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.25 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.153030779858625e-13.
Allowing negative dual variable(s) as small as -1.4308606383073297e-12.
Allowing negative dual variable(s) as small as -4.444274809278781e-13.
Allowing negative dual variable(s) as small as -4.4511963559479284e-13.
Allowing negative dual variable(s) as small as -1.2966054011714911e-12.
Allowing negative dual variable(s) as small as -1.0917407386110134e-12.
Allowing negative dual variable(s) as small as -1.0910146484160999e-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 -2.3941039711788254e-14.
Allowing negative dual variable(s) as small as -5.696115113143267e-12.
Allowing negative dual variable(s) as small as -2.0878937322852558e-11.
Allowing negative dual variable(s) as small as -2.088080902304399e-11.
Solving took 4 GP solves and 5.22 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.03 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Passed

Standard Output

Standard Error
