Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.018641752174702e-14.
Allowing negative dual variable(s) as small as -7.352885661449093e-14.
Allowing negative dual variable(s) as small as -1.5122408533740916e-13.
Allowing negative dual variable(s) as small as -1.5036756562114562e-13.
Solving took 4 GP solves and 2.41 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.934420927416028e-14.
Allowing negative dual variable(s) as small as -7.330767937130389e-14.
Allowing negative dual variable(s) as small as -1.5259321584082386e-13.
Allowing negative dual variable(s) as small as -1.5003840184157902e-13.
Solving took 4 GP solves and 1.78 seconds.
Allowing negative dual variable(s) as small as -5.182226175959315e-13.
Allowing negative dual variable(s) as small as -1.4298059264339358e-12.
Allowing negative dual variable(s) as small as -4.443129891784636e-13.
Allowing negative dual variable(s) as small as -4.4413084321348606e-13.
Allowing negative dual variable(s) as small as -1.2971884850998538e-12.
Allowing negative dual variable(s) as small as -1.0929133032605565e-12.
Allowing negative dual variable(s) as small as -1.0900691157014752e-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
Allowing negative dual variable(s) as small as -1.2750217548429532e-15.
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 -2.5018248144986516e-14.
Allowing negative dual variable(s) as small as -5.695986038318767e-12.
Allowing negative dual variable(s) as small as -2.0878957385595537e-11.
Allowing negative dual variable(s) as small as -2.0880635908223705e-11.
Solving took 4 GP solves and 5.34 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.22 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.171123945713063e-13.
Allowing negative dual variable(s) as small as -1.4306958395771119e-12.
Allowing negative dual variable(s) as small as -4.461986335968504e-13.
Allowing negative dual variable(s) as small as -4.4417594602386146e-13.
Allowing negative dual variable(s) as small as -1.297602975590395e-12.
Allowing negative dual variable(s) as small as -1.0910952046375155e-12.
Allowing negative dual variable(s) as small as -1.0905641624134321e-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 -2.4856062511411e-14.
Allowing negative dual variable(s) as small as -5.6960462415031305e-12.
Allowing negative dual variable(s) as small as -2.0878933031942466e-11.
Allowing negative dual variable(s) as small as -2.0880845071204508e-11.
Solving took 4 GP solves and 1.56 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
Passed

Standard Output

Standard Error
