Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.41836107232e-13.
Allowing negative dual variable(s) as small as -3.27885288365e-13.
Allowing negative dual variable(s) as small as -5.49356567181e-13.
Allowing negative dual variable(s) as small as -5.34959663373e-13.
Solving took 4 GP solves and 3.94 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 -5.4349233447e-13.
Allowing negative dual variable(s) as small as -3.51075071792e-13.
Allowing negative dual variable(s) as small as -5.23184794099e-13.
Allowing negative dual variable(s) as small as -5.42363029488e-13.
Solving took 4 GP solves and 2.26 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 -8.57051409009e-13.
Allowing negative dual variable(s) as small as -7.7240124019e-13.
Allowing negative dual variable(s) as small as -7.3824540231e-13.
Allowing negative dual variable(s) as small as -7.408457528e-13.
Allowing negative dual variable(s) as small as -7.41481528954e-13.
Allowing negative dual variable(s) as small as -1.52242780015e-12.
Allowing negative dual variable(s) as small as -1.048737811e-12.
Allowing negative dual variable(s) as small as -1.06168611229e-12.
Allowing negative dual variable(s) as small as -1.06121654433e-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 -1.47830966218e-12.
Allowing negative dual variable(s) as small as -1.14118458606e-13.
Allowing negative dual variable(s) as small as -6.22787411919e-15.
Allowing negative dual variable(s) as small as -1.62398740289e-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 -1.53889734657e-14.
Allowing negative dual variable(s) as small as -1.0815360907e-12.
Solving took 4 GP solves and 3.29 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 6.36 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -8.57220544548e-13.
Allowing negative dual variable(s) as small as -7.7215664418e-13.
Allowing negative dual variable(s) as small as -7.38382445464e-13.
Allowing negative dual variable(s) as small as -7.41271627414e-13.
Allowing negative dual variable(s) as small as -7.40908202845e-13.
Allowing negative dual variable(s) as small as -1.51644235363e-12.
Allowing negative dual variable(s) as small as -1.04902263091e-12.
Allowing negative dual variable(s) as small as -1.06085095136e-12.
Allowing negative dual variable(s) as small as -1.06350431933e-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 -1.48135605345e-12.
Allowing negative dual variable(s) as small as -1.14266885884e-13.
Allowing negative dual variable(s) as small as -6.471819608e-15.
Allowing negative dual variable(s) as small as -1.61040451807e-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 -1.54742659777e-14.
Allowing negative dual variable(s) as small as -1.08131135963e-12.
Solving took 4 GP solves and 4.45 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 1.56 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Passed

Standard Output

Standard Error
