Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.963410746797406e-14.
Allowing negative dual variable(s) as small as -7.680206297322467e-14.
Allowing negative dual variable(s) as small as -1.2939096408898232e-13.
Allowing negative dual variable(s) as small as -1.2479969314915795e-13.
Solving took 4 GP solves and 3.39 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.111238681245524e-14.
Allowing negative dual variable(s) as small as -7.036819044126119e-14.
Allowing negative dual variable(s) as small as -1.326566894527259e-13.
Allowing negative dual variable(s) as small as -1.2594547800504063e-13.
Solving took 4 GP solves and 4.53 seconds.
Allowing negative dual variable(s) as small as -5.856586916819229e-13.
Allowing negative dual variable(s) as small as -3.4081591715473536e-13.
Allowing negative dual variable(s) as small as -1.0227066589429956e-12.
Allowing negative dual variable(s) as small as -1.0228549778001916e-12.
Allowing negative dual variable(s) as small as -2.8157608623208263e-13.
Allowing negative dual variable(s) as small as -1.1550333985695799e-12.
Allowing negative dual variable(s) as small as -1.1170820941441145e-12.
Allowing negative dual variable(s) as small as -1.1162738485295809e-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 -1.2102344408744525e-12.
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 -6.145429020015363e-11.
Allowing negative dual variable(s) as small as -1.454847381243504e-12.
Allowing negative dual variable(s) as small as -6.463342264062805e-12.
Allowing negative dual variable(s) as small as -6.468656748806003e-12.
Solving took 4 GP solves and 6.16 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.83 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.846998232805767e-13.
Allowing negative dual variable(s) as small as -3.4043341062828247e-13.
Allowing negative dual variable(s) as small as -1.0225058647006513e-12.
Allowing negative dual variable(s) as small as -1.0230124039556365e-12.
Allowing negative dual variable(s) as small as -2.7544812134308594e-13.
Allowing negative dual variable(s) as small as -1.153903144909818e-12.
Allowing negative dual variable(s) as small as -1.1174249459761088e-12.
Allowing negative dual variable(s) as small as -1.116268048047958e-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 -1.208905967952506e-12.
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 -6.145446352305285e-11.
Allowing negative dual variable(s) as small as -1.4546655995556333e-12.
Allowing negative dual variable(s) as small as -6.463157909432948e-12.
Allowing negative dual variable(s) as small as -6.468917722833426e-12.
Solving took 4 GP solves and 4.5 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 3.55 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Passed

Standard Output

Standard Error
