Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.59067721873e-13.
Solving took 4 GP solves and 4.87 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.30956527945e-13.
Solving took 4 GP solves and 4.77 seconds.
Allowing negative dual variable(s) as small as -3.60135098826e-12.
Allowing negative dual variable(s) as small as -1.58798755395e-12.
Allowing negative dual variable(s) as small as -1.77602984403e-12.
Allowing negative dual variable(s) as small as -7.78103276255e-13.
Allowing negative dual variable(s) as small as -7.78166593662e-13.
Allowing negative dual variable(s) as small as -2.8580219788e-13.
Allowing negative dual variable(s) as small as -1.09840879881e-12.
Allowing negative dual variable(s) as small as -1.06951773826e-12.
Allowing negative dual variable(s) as small as -1.06277573547e-12.
MTOW [lbs] = 141.59
Zero fuel weight [lbs] = 53.63
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 = 21.754
speed at top of climb [m/s] = 26.532
design loiter speed [m/s] = 25.052
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -2.27406938766e-12.
Allowing negative dual variable(s) as small as -7.23811201947e-14.
Allowing negative dual variable(s) as small as -1.20998805593e-13.
Allowing negative dual variable(s) as small as -1.21442027441e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.190
optimum loiter speed for min power, end of loiter [m/s] = 17.170
optimum cruise speed, inbound [m/s] = 35.882
optimum cruise speed, outbound [m/s] = 25.488
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.64162118765e-12.
Allowing negative dual variable(s) as small as -1.97754766024e-12.
Allowing negative dual variable(s) as small as -1.99782615442e-12.
Solving took 4 GP solves and 8.64 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.85510807305e-12.
Solving took 4 GP solves and 1.28 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -3.60071000793e-12.
Allowing negative dual variable(s) as small as -1.59041616682e-12.
Allowing negative dual variable(s) as small as -1.77645832072e-12.
Allowing negative dual variable(s) as small as -7.78518742528e-13.
Allowing negative dual variable(s) as small as -7.7870435794e-13.
Allowing negative dual variable(s) as small as -2.77227026058e-13.
Allowing negative dual variable(s) as small as -1.09890384552e-12.
Allowing negative dual variable(s) as small as -1.06831102124e-12.
Allowing negative dual variable(s) as small as -1.06219416943e-12.
MTOW [lbs] = 141.59
Zero fuel weight [lbs] = 53.63
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 = 21.754
speed at top of climb [m/s] = 26.532
design loiter speed [m/s] = 25.052
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -2.27122812745e-12.
Allowing negative dual variable(s) as small as -7.30652517655e-14.
Allowing negative dual variable(s) as small as -1.2140657403e-13.
Allowing negative dual variable(s) as small as -1.20306759346e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.190
optimum loiter speed for min power, end of loiter [m/s] = 17.170
optimum cruise speed, inbound [m/s] = 35.882
optimum cruise speed, outbound [m/s] = 25.488
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.64181502606e-12.
Allowing negative dual variable(s) as small as -1.97635351203e-12.
Allowing negative dual variable(s) as small as -1.99579957129e-12.
Solving took 4 GP solves and 1.64 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.8471092631e-12.
Solving took 4 GP solves and 1.29 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Passed

Standard Output

Standard Error
