Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.00151265889e-12.
Allowing negative dual variable(s) as small as -4.97079547662e-12.
Allowing negative dual variable(s) as small as -4.81741816577e-12.
Allowing negative dual variable(s) as small as -1.07090755534e-11.
Solving took 4 GP solves and 3.21 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 1155331.2268 but bound is 1000000.0000
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.17319088472e-11.
Allowing negative dual variable(s) as small as -4.9866165884e-12.
Allowing negative dual variable(s) as small as -4.74624116051e-12.
Allowing negative dual variable(s) as small as -1.96318317505e-11.
Solving took 4 GP solves and 2.15 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 1155331.2266 but bound is 1000000.0000
Allowing negative dual variable(s) as small as -1.61192448278e-11.
Allowing negative dual variable(s) as small as -6.09656769512e-12.
Allowing negative dual variable(s) as small as -1.16350193369e-11.
Allowing negative dual variable(s) as small as -6.61098953358e-12.
Allowing negative dual variable(s) as small as -6.60248938855e-12.
Allowing negative dual variable(s) as small as -1.1016410657e-11.
Allowing negative dual variable(s) as small as -1.16865960268e-11.
Allowing negative dual variable(s) as small as -1.10531786631e-11.
Allowing negative dual variable(s) as small as -1.11135189593e-11.
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 -1.79814702624e-11.
Allowing negative dual variable(s) as small as -6.27843740539e-12.
Allowing negative dual variable(s) as small as -1.04098159129e-11.
Allowing negative dual variable(s) as small as -1.04264245892e-11.
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 -5.91618283955e-12.
Allowing negative dual variable(s) as small as -1.24752920572e-13.
Allowing negative dual variable(s) as small as -8.83637706886e-14.
Allowing negative dual variable(s) as small as -9.09064611053e-14.
Solving took 4 GP solves and 2.13 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.
Allowing negative dual variable(s) as small as -9.91170431321e-11.
Allowing negative dual variable(s) as small as -8.93001228519e-11.
Allowing negative dual variable(s) as small as -8.9873285463e-11.
Allowing negative dual variable(s) as small as -8.47969056084e-11.
Solving took 4 GP solves and 4.16 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -1.60955276884e-11.
Allowing negative dual variable(s) as small as -6.10941158774e-12.
Allowing negative dual variable(s) as small as -1.16473497513e-11.
Allowing negative dual variable(s) as small as -6.58779975016e-12.
Allowing negative dual variable(s) as small as -6.59586968377e-12.
Allowing negative dual variable(s) as small as -1.10145009433e-11.
Allowing negative dual variable(s) as small as -1.16871137334e-11.
Allowing negative dual variable(s) as small as -1.10536268723e-11.
Allowing negative dual variable(s) as small as -1.11199708296e-11.
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 -1.79864035992e-11.
Allowing negative dual variable(s) as small as -6.27684904921e-12.
Allowing negative dual variable(s) as small as -1.04091855578e-11.
Allowing negative dual variable(s) as small as -1.04288327106e-11.
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 -5.91624591216e-12.
Allowing negative dual variable(s) as small as -1.25449883792e-13.
Allowing negative dual variable(s) as small as -8.84627929695e-14.
Allowing negative dual variable(s) as small as -9.08968288584e-14.
Solving took 4 GP solves and 1.94 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.
Allowing negative dual variable(s) as small as -9.91034220833e-11.
Allowing negative dual variable(s) as small as -8.93121770117e-11.
Allowing negative dual variable(s) as small as -8.98735426358e-11.
Allowing negative dual variable(s) as small as -8.47875927454e-11.
Solving took 4 GP solves and 4.34 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Passed

Standard Output

Standard Error
