Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.0382970525e-13.
Allowing negative dual variable(s) as small as -1.08048986425e-13.
Allowing negative dual variable(s) as small as -5.33861149732e-16.
Allowing negative dual variable(s) as small as -1.07509487424e-15.
Solving took 4 GP solves and 1.8 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.2125673729e-13.
Allowing negative dual variable(s) as small as -1.02333072571e-13.
Allowing negative dual variable(s) as small as -1.1063198968e-15.
Allowing negative dual variable(s) as small as -3.52148865623e-16.
Solving took 4 GP solves and 1.65 seconds.
Allowing negative dual variable(s) as small as -3.88191475492e-12.
Allowing negative dual variable(s) as small as -1.71226314377e-12.
Allowing negative dual variable(s) as small as -7.75850737822e-13.
Allowing negative dual variable(s) as small as -7.70117476734e-13.
Allowing negative dual variable(s) as small as -7.70399369299e-13.
Allowing negative dual variable(s) as small as -2.47589275471e-13.
Allowing negative dual variable(s) as small as -1.01634076589e-12.
Allowing negative dual variable(s) as small as -1.0581692857e-12.
Allowing negative dual variable(s) as small as -1.04647291266e-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 -2.6676317405e-13.
Allowing negative dual variable(s) as small as -1.48772812646e-13.
Allowing negative dual variable(s) as small as -1.47165808186e-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 -4.00586856794e-13.
Allowing negative dual variable(s) as small as -2.223094086e-16.
Allowing negative dual variable(s) as small as -8.62151001467e-14.
Allowing negative dual variable(s) as small as -9.06218318829e-14.
Solving took 4 GP solves and 2.15 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 1.81 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -3.88128244821e-12.
Allowing negative dual variable(s) as small as -1.71225707224e-12.
Allowing negative dual variable(s) as small as -7.75731041902e-13.
Allowing negative dual variable(s) as small as -7.70152171203e-13.
Allowing negative dual variable(s) as small as -7.69927524513e-13.
Allowing negative dual variable(s) as small as -2.518458532e-13.
Allowing negative dual variable(s) as small as -1.01765883047e-12.
Allowing negative dual variable(s) as small as -1.05794789162e-12.
Allowing negative dual variable(s) as small as -1.04914102579e-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 -2.60686437714e-13.
Allowing negative dual variable(s) as small as -1.48336529691e-13.
Allowing negative dual variable(s) as small as -1.46977373848e-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 -4.00205820293e-13.
Allowing negative dual variable(s) as small as -1.21741843223e-15.
Allowing negative dual variable(s) as small as -8.77984318888e-14.
Allowing negative dual variable(s) as small as -8.93076925584e-14.
Solving took 4 GP solves and 2.3 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 1.3 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Passed

Standard Output

Standard Error
