Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.05242549186935e-14.
Allowing negative dual variable(s) as small as -7.477872487893222e-14.
Allowing negative dual variable(s) as small as -1.4966196684729205e-13.
Allowing negative dual variable(s) as small as -1.4933844091902237e-13.
Solving took 4 GP solves and 5.11 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.075844258795037e-14.
Allowing negative dual variable(s) as small as -7.198798848695454e-14.
Allowing negative dual variable(s) as small as -1.5141837436671857e-13.
Allowing negative dual variable(s) as small as -1.4800747433207917e-13.
Solving took 4 GP solves and 7.82 seconds.
Allowing negative dual variable(s) as small as -5.165121802486183e-13.
Allowing negative dual variable(s) as small as -1.4300054196336731e-12.
Allowing negative dual variable(s) as small as -4.4451942127210486e-13.
Allowing negative dual variable(s) as small as -4.460216918023008e-13.
Allowing negative dual variable(s) as small as -1.2975512591467675e-12.
Allowing negative dual variable(s) as small as -1.0909376700618534e-12.
Allowing negative dual variable(s) as small as -1.0901979189195665e-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 -2.547750856195485e-14.
Allowing negative dual variable(s) as small as -5.695956819414326e-12.
Allowing negative dual variable(s) as small as -2.0878967297839784e-11.
Allowing negative dual variable(s) as small as -2.08807863950882e-11.
Solving took 4 GP solves and 18.1 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 11.6 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.167706540465389e-13.
Allowing negative dual variable(s) as small as -1.4295509220829672e-12.
Allowing negative dual variable(s) as small as -4.452133106624956e-13.
Allowing negative dual variable(s) as small as -4.456400526375859e-13.
Allowing negative dual variable(s) as small as -1.2987224143334863e-12.
Allowing negative dual variable(s) as small as -1.0908361887385087e-12.
Allowing negative dual variable(s) as small as -1.0910358987786806e-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 -2.5018715495415164e-14.
Allowing negative dual variable(s) as small as -5.696121265275912e-12.
Allowing negative dual variable(s) as small as -2.0878829723277886e-11.
Allowing negative dual variable(s) as small as -2.0880745178464986e-11.
Solving took 4 GP solves and 6.76 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 9.04 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Passed

Standard Output

Standard Error
