Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.66115208667e-14.
Allowing negative dual variable(s) as small as -1.16564136815e-12.
Allowing negative dual variable(s) as small as -1.13312050715e-12.
Allowing negative dual variable(s) as small as -1.13491898171e-12.
Solving took 4 GP solves and 2.46 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.66709351458e-14.
Allowing negative dual variable(s) as small as -1.17022060445e-12.
Allowing negative dual variable(s) as small as -1.14674806109e-12.
Allowing negative dual variable(s) as small as -1.13486954209e-12.
Solving took 4 GP solves and 1.98 seconds.
Allowing negative dual variable(s) as small as -1.56990306172e-12.
Allowing negative dual variable(s) as small as -3.96023058097e-12.
Allowing negative dual variable(s) as small as -1.78656828914e-12.
Allowing negative dual variable(s) as small as -2.08238721405e-12.
Allowing negative dual variable(s) as small as -2.08063774543e-12.
Allowing negative dual variable(s) as small as -4.7178710591e-13.
Allowing negative dual variable(s) as small as -8.94438169363e-13.
Allowing negative dual variable(s) as small as -9.42012852272e-13.
Allowing negative dual variable(s) as small as -9.44138864312e-13.
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 = 21.712
speed at top of climb [m/s] = 26.507
design loiter speed [m/s] = 25.048
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 -2.29480930786e-13.
Allowing negative dual variable(s) as small as -9.13025080887e-14.
Allowing negative dual variable(s) as small as -1.20024758361e-13.
Allowing negative dual variable(s) as small as -1.20233358859e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.166
optimum loiter speed for min power, end of loiter [m/s] = 17.158
optimum cruise speed, inbound [m/s] = 35.697
optimum cruise speed, outbound [m/s] = 25.443
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.61167507322e-13.
Allowing negative dual variable(s) as small as -2.01708892709e-12.
Allowing negative dual variable(s) as small as -1.25475019177e-14.
Allowing negative dual variable(s) as small as -1.69990581081e-14.
Solving took 4 GP solves and 2.84 seconds.
Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1021559.0193 but bound is 1000000.0000
Max Speed [m/s]: 73.83
Beginning signomial solve.
Solving took 4 GP solves and 2.3 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56950320795e-12.
Allowing negative dual variable(s) as small as -3.96094962385e-12.
Allowing negative dual variable(s) as small as -1.78652231897e-12.
Allowing negative dual variable(s) as small as -2.08231782511e-12.
Allowing negative dual variable(s) as small as -2.08100030263e-12.
Allowing negative dual variable(s) as small as -4.71276013006e-13.
Allowing negative dual variable(s) as small as -8.93877094739e-13.
Allowing negative dual variable(s) as small as -9.4186247343e-13.
Allowing negative dual variable(s) as small as -9.44283280041e-13.
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 = 21.712
speed at top of climb [m/s] = 26.507
design loiter speed [m/s] = 25.048
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 -2.36431534073e-13.
Allowing negative dual variable(s) as small as -9.27585916063e-14.
Allowing negative dual variable(s) as small as -1.2012385444e-13.
Allowing negative dual variable(s) as small as -1.2070791415e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.166
optimum loiter speed for min power, end of loiter [m/s] = 17.158
optimum cruise speed, inbound [m/s] = 35.697
optimum cruise speed, outbound [m/s] = 25.443
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.61669080634e-13.
Allowing negative dual variable(s) as small as -2.01698796799e-12.
Allowing negative dual variable(s) as small as -1.3117182185e-14.
Allowing negative dual variable(s) as small as -1.77487058775e-14.
Solving took 4 GP solves and 2.62 seconds.
Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1021559.0193 but bound is 1000000.0000
Max Speed [m/s]: 73.83
Beginning signomial solve.
Solving took 4 GP solves and 1.64 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Passed

Standard Output

Standard Error
