Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.02926693346506e-14.
Allowing negative dual variable(s) as small as -7.520373213054654e-14.
Allowing negative dual variable(s) as small as -1.513637305772253e-13.
Allowing negative dual variable(s) as small as -1.5147041607099787e-13.
Solving took 4 GP solves and 6.82 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.454447657426975e-14.
Allowing negative dual variable(s) as small as -8.123363093304192e-14.
Allowing negative dual variable(s) as small as -1.5141013443020768e-13.
Allowing negative dual variable(s) as small as -1.4886139196312875e-13.
Solving took 4 GP solves and 23.7 seconds.
Allowing negative dual variable(s) as small as -5.176276074436714e-13.
Allowing negative dual variable(s) as small as -1.4316863666818946e-12.
Allowing negative dual variable(s) as small as -4.424516308887405e-13.
Allowing negative dual variable(s) as small as -4.4336929960753224e-13.
Allowing negative dual variable(s) as small as -1.2984123325121555e-12.
Allowing negative dual variable(s) as small as -1.0922827312770389e-12.
Allowing negative dual variable(s) as small as -1.090798350082689e-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 -2.423894268164525e-14.
Allowing negative dual variable(s) as small as -5.696037278041664e-12.
Allowing negative dual variable(s) as small as -2.0879025499564702e-11.
Allowing negative dual variable(s) as small as -2.088085637732088e-11.
Solving took 4 GP solves and 5.77 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 4.81 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.157107380027171e-13.
Allowing negative dual variable(s) as small as -1.4291831607060601e-12.
Allowing negative dual variable(s) as small as -4.448542229029684e-13.
Allowing negative dual variable(s) as small as -4.433207273502049e-13.
Allowing negative dual variable(s) as small as -1.2973334429303152e-12.
Allowing negative dual variable(s) as small as -1.0899360840949113e-12.
Allowing negative dual variable(s) as small as -1.0909163112790554e-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 -2.4951838326702056e-14.
Allowing negative dual variable(s) as small as -5.696010269496168e-12.
Allowing negative dual variable(s) as small as -2.0879057432918572e-11.
Allowing negative dual variable(s) as small as -2.0880778863403582e-11.
Solving took 4 GP solves and 2.26 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 6.71 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Passed

Standard Output

Standard Error
