Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.1159597391770006e-14.
Allowing negative dual variable(s) as small as -7.646010560802274e-14.
Allowing negative dual variable(s) as small as -1.5284778651092346e-13.
Allowing negative dual variable(s) as small as -1.490439716089753e-13.
Solving took 4 GP solves and 17.5 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.030090927116149e-14.
Allowing negative dual variable(s) as small as -7.577879296283285e-14.
Allowing negative dual variable(s) as small as -1.5132166353293286e-13.
Allowing negative dual variable(s) as small as -1.4886052460139076e-13.
Solving took 4 GP solves and 9.78 seconds.
Allowing negative dual variable(s) as small as -5.175183198646849e-13.
Allowing negative dual variable(s) as small as -1.4298943973312106e-12.
Allowing negative dual variable(s) as small as -4.4287490341687885e-13.
Allowing negative dual variable(s) as small as -4.4380124575305047e-13.
Allowing negative dual variable(s) as small as -1.296564743590023e-12.
Allowing negative dual variable(s) as small as -1.0908374897811157e-12.
Allowing negative dual variable(s) as small as -1.0919081394264452e-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] = 25.637
optimum cruise speed, outbound [m/s] = 36.269
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.4711100128147596e-14.
Allowing negative dual variable(s) as small as -5.695948150561506e-12.
Allowing negative dual variable(s) as small as -2.087895733607058e-11.
Allowing negative dual variable(s) as small as -2.0880760546792553e-11.
Solving took 4 GP solves and 7.25 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 6.34 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.160021715466812e-13.
Allowing negative dual variable(s) as small as -1.4302517503672618e-12.
Allowing negative dual variable(s) as small as -4.4475360894136173e-13.
Allowing negative dual variable(s) as small as -4.430362327001447e-13.
Allowing negative dual variable(s) as small as -1.2973295398024942e-12.
Allowing negative dual variable(s) as small as -1.0911851934178318e-12.
Allowing negative dual variable(s) as small as -1.0905992905638207e-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] = 25.637
optimum cruise speed, outbound [m/s] = 36.269
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.480258243930814e-14.
Allowing negative dual variable(s) as small as -5.696021410838161e-12.
Allowing negative dual variable(s) as small as -2.0878984631548486e-11.
Allowing negative dual variable(s) as small as -2.0880825391029253e-11.
Solving took 4 GP solves and 32.8 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 7.39 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417

Passed

Standard Output

Standard Error