Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.52201080001e-13.
Allowing negative dual variable(s) as small as -3.20114594554e-13.
Allowing negative dual variable(s) as small as -5.37497563818e-13.
Allowing negative dual variable(s) as small as -5.28841727354e-13.
Solving took 4 GP solves and 2.51 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 -5.46292178161e-13.
Allowing negative dual variable(s) as small as -3.22011080994e-13.
Allowing negative dual variable(s) as small as -5.23831845956e-13.
Allowing negative dual variable(s) as small as -5.40713307462e-13.
Solving took 4 GP solves and 7.68 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 -8.57272586252e-13.
Allowing negative dual variable(s) as small as -7.72746450162e-13.
Allowing negative dual variable(s) as small as -7.38301780823e-13.
Allowing negative dual variable(s) as small as -7.41539642191e-13.
Allowing negative dual variable(s) as small as -7.41259484349e-13.
Allowing negative dual variable(s) as small as -1.52096824718e-12.
Allowing negative dual variable(s) as small as -1.04769177275e-12.
Allowing negative dual variable(s) as small as -1.06109489684e-12.
Allowing negative dual variable(s) as small as -1.06259836e-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 -1.47815288655e-12.
Allowing negative dual variable(s) as small as -1.1523822261e-13.
Allowing negative dual variable(s) as small as -4.94244402349e-15.
Allowing negative dual variable(s) as small as -1.59921663585e-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 -1.51948795716e-14.
Allowing negative dual variable(s) as small as -1.08072812927e-12.
Solving took 4 GP solves and 1.78 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 5.42 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -8.56896151258e-13.
Allowing negative dual variable(s) as small as -7.72254656056e-13.
Allowing negative dual variable(s) as small as -7.38409333678e-13.
Allowing negative dual variable(s) as small as -7.40908202845e-13.
Allowing negative dual variable(s) as small as -7.41086012002e-13.
Allowing negative dual variable(s) as small as -1.5178643932e-12.
Allowing negative dual variable(s) as small as -1.04818345843e-12.
Allowing negative dual variable(s) as small as -1.06197060694e-12.
Allowing negative dual variable(s) as small as -1.06072344918e-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 -1.4809546818e-12.
Allowing negative dual variable(s) as small as -1.14535984863e-13.
Allowing negative dual variable(s) as small as -5.81110680409e-15.
Allowing negative dual variable(s) as small as -1.60710637506e-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 -1.43675095413e-14.
Allowing negative dual variable(s) as small as -1.08064358871e-12.
Solving took 4 GP solves and 8.35 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 23.8 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Passed

Standard Output

Standard Error
