Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.056849036733091e-14.
Allowing negative dual variable(s) as small as -7.261465734265116e-14.
Allowing negative dual variable(s) as small as -1.5078173085103508e-13.
Allowing negative dual variable(s) as small as -1.4982893398185482e-13.
Solving took 4 GP solves and 1.63 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.063224145507306e-14.
Allowing negative dual variable(s) as small as -7.448252084540918e-14.
Allowing negative dual variable(s) as small as -1.4943168230585613e-13.
Allowing negative dual variable(s) as small as -1.478778037522499e-13.
Solving took 4 GP solves and 1.72 seconds.
Allowing negative dual variable(s) as small as -5.164531996504351e-13.
Allowing negative dual variable(s) as small as -1.430017562698005e-12.
Allowing negative dual variable(s) as small as -4.439486972485085e-13.
Allowing negative dual variable(s) as small as -4.453781093927134e-13.
Allowing negative dual variable(s) as small as -1.2964288930578105e-12.
Allowing negative dual variable(s) as small as -1.0923293519704558e-12.
Allowing negative dual variable(s) as small as -1.0914268620820788e-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 -2.393536268521752e-14.
Allowing negative dual variable(s) as small as -5.696031062037441e-12.
Allowing negative dual variable(s) as small as -2.0878912886137318e-11.
Allowing negative dual variable(s) as small as -2.0880805612730526e-11.
Solving took 4 GP solves and 2.05 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.3 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.159640076302097e-13.
Allowing negative dual variable(s) as small as -1.430987273121076e-12.
Allowing negative dual variable(s) as small as -4.427500033266085e-13.
Allowing negative dual variable(s) as small as -4.431090910861357e-13.
Allowing negative dual variable(s) as small as -1.2972240469311114e-12.
Allowing negative dual variable(s) as small as -1.0930568516281935e-12.
Allowing negative dual variable(s) as small as -1.0914332588748965e-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 -2.4128402870325313e-14.
Allowing negative dual variable(s) as small as -5.6960723029069725e-12.
Allowing negative dual variable(s) as small as -2.0878882800665232e-11.
Allowing negative dual variable(s) as small as -2.0880874792373018e-11.
Solving took 4 GP solves and 1.84 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.88 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Passed

Standard Output

Standard Error
