Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.16109332891e-14.
Allowing negative dual variable(s) as small as -8.20350731789e-14.
Allowing negative dual variable(s) as small as -1.55269460483e-13.
Allowing negative dual variable(s) as small as -1.48002703843e-13.
Solving took 4 GP solves and 12.1 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.17744309767e-14.
Allowing negative dual variable(s) as small as -8.09313553674e-14.
Allowing negative dual variable(s) as small as -1.51803049298e-13.
Allowing negative dual variable(s) as small as -1.49519285841e-13.
Solving took 4 GP solves and 242 seconds.
Allowing negative dual variable(s) as small as -5.22960147409e-13.
Allowing negative dual variable(s) as small as -5.13034059679e-13.
Allowing negative dual variable(s) as small as -5.15185116789e-13.
Allowing negative dual variable(s) as small as -5.15570225401e-13.
Allowing negative dual variable(s) as small as -2.33204081046e-13.
Allowing negative dual variable(s) as small as -1.91421314563e-14.
Allowing negative dual variable(s) as small as -1.25849146642e-12.
Allowing negative dual variable(s) as small as -1.26004729654e-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 -1.83338587367e-14.
Allowing negative dual variable(s) as small as -1.14268186927e-13.
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 -5.43412775039e-11.
Allowing negative dual variable(s) as small as -6.44963029762e-12.
Allowing negative dual variable(s) as small as -1.93392188544e-11.
Allowing negative dual variable(s) as small as -1.93545643939e-11.
Solving took 4 GP solves and 489 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 43.6 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.25043550303e-13.
Allowing negative dual variable(s) as small as -5.11266376457e-13.
Allowing negative dual variable(s) as small as -5.14414899566e-13.
Allowing negative dual variable(s) as small as -5.15303077986e-13.
Allowing negative dual variable(s) as small as -2.3939921226e-13.
Allowing negative dual variable(s) as small as -1.91353009826e-14.
Allowing negative dual variable(s) as small as -1.25958586009e-12.
Allowing negative dual variable(s) as small as -1.26008296679e-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 -1.3466658344e-14.
Allowing negative dual variable(s) as small as -1.13298259663e-13.
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 -5.43412522683e-11.
Allowing negative dual variable(s) as small as -6.44960500548e-12.
Allowing negative dual variable(s) as small as -1.93391791653e-11.
Allowing negative dual variable(s) as small as -1.9354425488e-11.
Solving took 4 GP solves and 6.64 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 22.5 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Passed

Standard Output

Standard Error
