Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.6375598474e-14.
Allowing negative dual variable(s) as small as -1.18723217021e-12.
Allowing negative dual variable(s) as small as -1.13446448416e-12.
Allowing negative dual variable(s) as small as -1.1117764695e-12.
Solving took 4 GP solves and 7.34 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.52779521946e-14.
Allowing negative dual variable(s) as small as -1.18534218899e-12.
Allowing negative dual variable(s) as small as -1.13956023437e-12.
Allowing negative dual variable(s) as small as -1.13494847201e-12.
Solving took 4 GP solves and 2.13 seconds.
Allowing negative dual variable(s) as small as -1.57007306462e-12.
Allowing negative dual variable(s) as small as -3.96046910545e-12.
Allowing negative dual variable(s) as small as -1.787378405e-12.
Allowing negative dual variable(s) as small as -2.08232129456e-12.
Allowing negative dual variable(s) as small as -2.08063687807e-12.
Allowing negative dual variable(s) as small as -4.74151100327e-13.
Allowing negative dual variable(s) as small as -8.92368752677e-13.
Allowing negative dual variable(s) as small as -9.41076535275e-13.
Allowing negative dual variable(s) as small as -9.42659036766e-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 -2.39716449815e-13.
Allowing negative dual variable(s) as small as -9.32167754444e-14.
Allowing negative dual variable(s) as small as -1.19906363484e-13.
Allowing negative dual variable(s) as small as -1.19852478636e-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 -9.6116007609e-13.
Allowing negative dual variable(s) as small as -2.01709978735e-12.
Allowing negative dual variable(s) as small as -1.26152400954e-14.
Allowing negative dual variable(s) as small as -1.78318643429e-14.
Solving took 4 GP solves and 3.73 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 4.56 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56920830496e-12.
Allowing negative dual variable(s) as small as -3.96091406202e-12.
Allowing negative dual variable(s) as small as -1.78683717128e-12.
Allowing negative dual variable(s) as small as -2.08237680571e-12.
Allowing negative dual variable(s) as small as -2.08071407326e-12.
Allowing negative dual variable(s) as small as -4.77189251655e-13.
Allowing negative dual variable(s) as small as -8.93292059247e-13.
Allowing negative dual variable(s) as small as -9.40585174851e-13.
Allowing negative dual variable(s) as small as -9.42892790755e-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 -2.35934752638e-13.
Allowing negative dual variable(s) as small as -9.29164514427e-14.
Allowing negative dual variable(s) as small as -1.19110450669e-13.
Allowing negative dual variable(s) as small as -1.19305715481e-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 -9.61286022478e-13.
Allowing negative dual variable(s) as small as -2.01716500277e-12.
Allowing negative dual variable(s) as small as -1.293366895e-14.
Allowing negative dual variable(s) as small as -1.72812288174e-14.
Solving took 4 GP solves and 4.89 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 3.72 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Passed

Standard Output

Standard Error
