Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.51571375379e-13.
Allowing negative dual variable(s) as small as -3.58207821044e-13.
Allowing negative dual variable(s) as small as -5.34050234591e-13.
Allowing negative dual variable(s) as small as -5.18564358121e-13.
Solving took 4 GP solves and 28.6 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 -5.54620585569e-13.
Allowing negative dual variable(s) as small as -3.36492552572e-13.
Allowing negative dual variable(s) as small as -5.37974179093e-13.
Allowing negative dual variable(s) as small as -5.20328571896e-13.
Solving took 4 GP solves and 33.1 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 -8.57169370205e-13.
Allowing negative dual variable(s) as small as -7.72592927134e-13.
Allowing negative dual variable(s) as small as -7.38496937214e-13.
Allowing negative dual variable(s) as small as -7.40963713997e-13.
Allowing negative dual variable(s) as small as -7.41314128139e-13.
Allowing negative dual variable(s) as small as -1.5185025546e-12.
Allowing negative dual variable(s) as small as -1.04814280085e-12.
Allowing negative dual variable(s) as small as -1.06288523989e-12.
Allowing negative dual variable(s) as small as -1.0624487401e-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 -1.47805834412e-12.
Allowing negative dual variable(s) as small as -1.14467138025e-13.
Allowing negative dual variable(s) as small as -6.11999600303e-15.
Allowing negative dual variable(s) as small as -1.60893325572e-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 -1.46245525947e-14.
Allowing negative dual variable(s) as small as -1.08149416935e-12.
Solving took 4 GP solves and 2.54 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 1.65 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -8.56747832401e-13.
Allowing negative dual variable(s) as small as -7.72563436835e-13.
Allowing negative dual variable(s) as small as -7.38706838754e-13.
Allowing negative dual variable(s) as small as -7.41046113362e-13.
Allowing negative dual variable(s) as small as -7.41023561956e-13.
Allowing negative dual variable(s) as small as -1.51801596467e-12.
Allowing negative dual variable(s) as small as -1.04915360254e-12.
Allowing negative dual variable(s) as small as -1.06202037182e-12.
Allowing negative dual variable(s) as small as -1.0609128593e-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 -1.47790590529e-12.
Allowing negative dual variable(s) as small as -1.13437579642e-13.
Allowing negative dual variable(s) as small as -5.82422565037e-15.
Allowing negative dual variable(s) as small as -1.60928020042e-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 -1.53877396563e-14.
Allowing negative dual variable(s) as small as -1.08174079922e-12.
Solving took 4 GP solves and 4.82 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 1.76 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Passed

Standard Output

Standard Error
