Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.46107863791e-13.
Allowing negative dual variable(s) as small as -3.12663957225e-13.
Allowing negative dual variable(s) as small as -5.37670602485e-13.
Allowing negative dual variable(s) as small as -5.14812584923e-13.
Solving took 4 GP solves and 27.4 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 -5.5342319269e-13.
Allowing negative dual variable(s) as small as -3.38813612583e-13.
Allowing negative dual variable(s) as small as -5.39286497403e-13.
Allowing negative dual variable(s) as small as -5.18082104994e-13.
Solving took 4 GP solves and 31.2 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 -8.57110389607e-13.
Allowing negative dual variable(s) as small as -7.72737776544e-13.
Allowing negative dual variable(s) as small as -7.38665205391e-13.
Allowing negative dual variable(s) as small as -7.4119009541e-13.
Allowing negative dual variable(s) as small as -7.40667076282e-13.
Allowing negative dual variable(s) as small as -1.51905029354e-12.
Allowing negative dual variable(s) as small as -1.04755483801e-12.
Allowing negative dual variable(s) as small as -1.06151014628e-12.
Allowing negative dual variable(s) as small as -1.06188441287e-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 -1.48480251531e-12.
Allowing negative dual variable(s) as small as -1.13415245077e-13.
Allowing negative dual variable(s) as small as -6.08172366634e-15.
Allowing negative dual variable(s) as small as -1.60098930641e-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 -1.57484062852e-14.
Allowing negative dual variable(s) as small as -1.08102105616e-12.
Solving took 4 GP solves and 2.24 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 1.72 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -8.57067888882e-13.
Allowing negative dual variable(s) as small as -7.72803696036e-13.
Allowing negative dual variable(s) as small as -7.38730257521e-13.
Allowing negative dual variable(s) as small as -7.41161472473e-13.
Allowing negative dual variable(s) as small as -7.41259484349e-13.
Allowing negative dual variable(s) as small as -1.5136095502e-12.
Allowing negative dual variable(s) as small as -1.04923643558e-12.
Allowing negative dual variable(s) as small as -1.06262373033e-12.
Allowing negative dual variable(s) as small as -1.06252691107e-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 -1.47788920858e-12.
Allowing negative dual variable(s) as small as -1.14341695834e-13.
Allowing negative dual variable(s) as small as -6.45805024041e-15.
Allowing negative dual variable(s) as small as -1.60933332632e-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 -1.45759611732e-14.
Allowing negative dual variable(s) as small as -1.08186563086e-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 1.68 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Passed

Standard Output

Standard Error
