Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.57431704962e-13.
Allowing negative dual variable(s) as small as -3.49089680773e-13.
Allowing negative dual variable(s) as small as -5.21880715726e-13.
Allowing negative dual variable(s) as small as -5.19405699007e-13.
Solving took 4 GP solves and 7.35 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 -5.46417078251e-13.
Allowing negative dual variable(s) as small as -3.35225337073e-13.
Allowing negative dual variable(s) as small as -5.12324991458e-13.
Allowing negative dual variable(s) as small as -5.23650567352e-13.
Solving took 4 GP solves and 4.04 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 -8.57424374556e-13.
Allowing negative dual variable(s) as small as -7.72571243091e-13.
Allowing negative dual variable(s) as small as -7.38826534674e-13.
Allowing negative dual variable(s) as small as -7.41504947721e-13.
Allowing negative dual variable(s) as small as -7.41064327958e-13.
Allowing negative dual variable(s) as small as -1.5158774843e-12.
Allowing negative dual variable(s) as small as -1.04847315725e-12.
Allowing negative dual variable(s) as small as -1.06212781625e-12.
Allowing negative dual variable(s) as small as -1.06173598559e-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 -1.48434411464e-12.
Allowing negative dual variable(s) as small as -1.14633129378e-13.
Allowing negative dual variable(s) as small as -6.25584653524e-15.
Allowing negative dual variable(s) as small as -1.6019368991e-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 -1.46050853423e-14.
Allowing negative dual variable(s) as small as -1.08191194881e-12.
Solving took 4 GP solves and 5.03 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 6.45 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -8.56912631131e-13.
Allowing negative dual variable(s) as small as -7.72449812447e-13.
Allowing negative dual variable(s) as small as -7.38332138484e-13.
Allowing negative dual variable(s) as small as -7.41039174468e-13.
Allowing negative dual variable(s) as small as -7.41132849535e-13.
Allowing negative dual variable(s) as small as -1.51784314284e-12.
Allowing negative dual variable(s) as small as -1.04712126556e-12.
Allowing negative dual variable(s) as small as -1.06256789392e-12.
Allowing negative dual variable(s) as small as -1.06271632119e-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 -1.48254433903e-12.
Allowing negative dual variable(s) as small as -1.14797602847e-13.
Allowing negative dual variable(s) as small as -6.05017338312e-15.
Allowing negative dual variable(s) as small as -1.60178944761e-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 -1.50413872489e-14.
Allowing negative dual variable(s) as small as -1.08128767545e-12.
Solving took 4 GP solves and 10.5 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 2.06 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Passed

Standard Output

Standard Error
