Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.2713571515e-13.
Allowing negative dual variable(s) as small as -2.76185758291e-13.
Solving took 4 GP solves and 1.28 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.26061487637e-13.
Allowing negative dual variable(s) as small as -2.81152271603e-13.
Solving took 4 GP solves and 1.28 seconds.
Allowing negative dual variable(s) as small as -2.37062886682e-12.
Allowing negative dual variable(s) as small as -2.69888278392e-13.
Allowing negative dual variable(s) as small as -1.09859528159e-12.
Allowing negative dual variable(s) as small as -1.10446591109e-12.
Allowing negative dual variable(s) as small as -1.0976745771e-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 -2.20892683485e-12.
Allowing negative dual variable(s) as small as -7.06833680128e-14.
Allowing negative dual variable(s) as small as -1.181576538e-13.
Allowing negative dual variable(s) as small as -1.18523029932e-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 -1.01246033897e-13.
Allowing negative dual variable(s) as small as -2.05757677035e-12.
Allowing negative dual variable(s) as small as -2.07824392179e-12.
Solving took 4 GP solves and 1.69 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.18511145878e-12.
Solving took 4 GP solves and 1.06 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -2.37233583472e-12.
Allowing negative dual variable(s) as small as -2.70529258717e-13.
Allowing negative dual variable(s) as small as -1.09715079903e-12.
Allowing negative dual variable(s) as small as -1.1052822069e-12.
Allowing negative dual variable(s) as small as -1.09652207019e-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 -2.2106383564e-12.
Allowing negative dual variable(s) as small as -6.94448838712e-14.
Allowing negative dual variable(s) as small as -1.18585154717e-13.
Allowing negative dual variable(s) as small as -1.17609481182e-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 -1.02734565924e-13.
Allowing negative dual variable(s) as small as -2.06251365498e-12.
Allowing negative dual variable(s) as small as -2.0764222057e-12.
Solving took 4 GP solves and 1.81 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.18219972542e-12.
Solving took 4 GP solves and 1.21 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Passed

Standard Output

Standard Error
