Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.57829390319e-13.
Allowing negative dual variable(s) as small as -3.25503513032e-13.
Allowing negative dual variable(s) as small as -5.40285698125e-13.
Allowing negative dual variable(s) as small as -5.36201725382e-13.
Solving took 4 GP solves and 2.15 seconds.
Warning: Variable [Re_Mission/Cruise/FlightSegment.1/AircraftPerf.1/TailAero.3_(0,)] could cause inaccurate result because it is above upper bound. Solution is 1155331.2270 but bound is 1000000.0000
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.4561823809e-13.
Allowing negative dual variable(s) as small as -3.2532266811e-13.
Allowing negative dual variable(s) as small as -5.50517964548e-13.
Allowing negative dual variable(s) as small as -5.18267286725e-13.
Solving took 4 GP solves and 5.36 seconds.
Warning: Variable [Re_Mission/Cruise/FlightSegment.1/AircraftPerf.1/TailAero.3_(0,)] could cause inaccurate result because it is above upper bound. Solution is 1155331.2270 but bound is 1000000.0000
Allowing negative dual variable(s) as small as -8.5737146549e-13.
Allowing negative dual variable(s) as small as -7.72728235565e-13.
Allowing negative dual variable(s) as small as -7.38427548275e-13.
Allowing negative dual variable(s) as small as -7.41014888339e-13.
Allowing negative dual variable(s) as small as -7.41478926869e-13.
Allowing negative dual variable(s) as small as -1.51944559365e-12.
Allowing negative dual variable(s) as small as -1.04569163658e-12.
Allowing negative dual variable(s) as small as -1.06119290872e-12.
Allowing negative dual variable(s) as small as -1.06192539571e-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 = 21.769
speed at top of climb [m/s] = 26.550
design loiter speed [m/s] = 25.056
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 -1.48484002871e-12.
Allowing negative dual variable(s) as small as -1.14457922307e-13.
Allowing negative dual variable(s) as small as -7.39295777374e-15.
Allowing negative dual variable(s) as small as -1.61188879085e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.207
optimum loiter speed for min power, end of loiter [m/s] = 17.178
optimum cruise speed, inbound [m/s] = 36.034
optimum cruise speed, outbound [m/s] = 25.521
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.48622252751e-14.
Allowing negative dual variable(s) as small as -1.08060787084e-12.
Solving took 4 GP solves and 2.32 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 1078212.3036 but bound is 1000000.0000
Max Speed [m/s]: 74.35
Beginning signomial solve.
Solving took 4 GP solves and 6.55 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -8.5737146549e-13.
Allowing negative dual variable(s) as small as -7.72157511542e-13.
Allowing negative dual variable(s) as small as -7.38362496144e-13.
Allowing negative dual variable(s) as small as -7.40869171567e-13.
Allowing negative dual variable(s) as small as -7.4136443512e-13.
Allowing negative dual variable(s) as small as -1.51874584957e-12.
Allowing negative dual variable(s) as small as -1.04774533233e-12.
Allowing negative dual variable(s) as small as -1.06254577619e-12.
Allowing negative dual variable(s) as small as -1.06344804924e-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 = 21.769
speed at top of climb [m/s] = 26.550
design loiter speed [m/s] = 25.056
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 -1.48079855669e-12.
Allowing negative dual variable(s) as small as -1.15287120128e-13.
Allowing negative dual variable(s) as small as -6.68584111685e-15.
Allowing negative dual variable(s) as small as -1.6166050703e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.207
optimum loiter speed for min power, end of loiter [m/s] = 17.178
optimum cruise speed, inbound [m/s] = 36.034
optimum cruise speed, outbound [m/s] = 25.521
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.4916336175e-14.
Allowing negative dual variable(s) as small as -1.08110258522e-12.
Solving took 4 GP solves and 8.57 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 1078212.3036 but bound is 1000000.0000
Max Speed [m/s]: 74.35
Beginning signomial solve.
Solving took 4 GP solves and 25.1 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Passed

Standard Output

Standard Error
