Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.24779093308e-13.
Allowing negative dual variable(s) as small as -7.20205145521e-13.
Solving took 4 GP solves and 1.2 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.24779093308e-13.
Allowing negative dual variable(s) as small as -7.20205145521e-13.
Solving took 4 GP solves and 1.57 seconds.
Allowing negative dual variable(s) as small as -2.37308610262e-12.
Allowing negative dual variable(s) as small as -2.67349293745e-13.
Allowing negative dual variable(s) as small as -1.09694284905e-12.
Allowing negative dual variable(s) as small as -1.10521401059e-12.
Allowing negative dual variable(s) as small as -1.09716955573e-12.
MTOW [lbs] = 141.59
Zero fuel weight [lbs] = 53.63
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 = 21.754
speed at top of climb [m/s] = 26.532
design loiter speed [m/s] = 25.052
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -2.212254685e-12.
Allowing negative dual variable(s) as small as -6.92270676547e-14.
Allowing negative dual variable(s) as small as -1.18663217273e-13.
Allowing negative dual variable(s) as small as -1.18107021559e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.190
optimum loiter speed for min power, end of loiter [m/s] = 17.170
optimum cruise speed, inbound [m/s] = 35.882
optimum cruise speed, outbound [m/s] = 25.488
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.00945968241e-13.
Allowing negative dual variable(s) as small as -2.06343111173e-12.
Allowing negative dual variable(s) as small as -2.07824307481e-12.
Solving took 4 GP solves and 2.48 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.18595973856e-12.
Solving took 4 GP solves and 2.03 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -2.37308610262e-12.
Allowing negative dual variable(s) as small as -2.67349293745e-13.
Allowing negative dual variable(s) as small as -1.09694284905e-12.
Allowing negative dual variable(s) as small as -1.10521401059e-12.
Allowing negative dual variable(s) as small as -1.09716955573e-12.
MTOW [lbs] = 141.59
Zero fuel weight [lbs] = 53.63
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 = 21.754
speed at top of climb [m/s] = 26.532
design loiter speed [m/s] = 25.052
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -2.212254685e-12.
Allowing negative dual variable(s) as small as -6.92270676547e-14.
Allowing negative dual variable(s) as small as -1.18663217273e-13.
Allowing negative dual variable(s) as small as -1.18107021559e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.190
optimum loiter speed for min power, end of loiter [m/s] = 17.170
optimum cruise speed, inbound [m/s] = 35.882
optimum cruise speed, outbound [m/s] = 25.488
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.00945968241e-13.
Allowing negative dual variable(s) as small as -2.06343111173e-12.
Allowing negative dual variable(s) as small as -2.07824307481e-12.
Solving took 4 GP solves and 2.45 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.18595973856e-12.
Solving took 4 GP solves and 1.95 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Passed

Standard Output

Standard Error
