Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.55870020152e-13.
Allowing negative dual variable(s) as small as -3.21922176416e-13.
Allowing negative dual variable(s) as small as -5.20642990526e-13.
Allowing negative dual variable(s) as small as -5.48804925116e-13.
Solving took 4 GP solves and 2.04 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 -5.67190825557e-13.
Allowing negative dual variable(s) as small as -3.38966701929e-13.
Allowing negative dual variable(s) as small as -5.25873181806e-13.
Allowing negative dual variable(s) as small as -5.4388655038e-13.
Solving took 4 GP solves and 4.55 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 -8.5693691726e-13.
Allowing negative dual variable(s) as small as -7.72083785794e-13.
Allowing negative dual variable(s) as small as -7.38487396235e-13.
Allowing negative dual variable(s) as small as -7.41046980723e-13.
Allowing negative dual variable(s) as small as -7.40909937569e-13.
Allowing negative dual variable(s) as small as -1.5175356631e-12.
Allowing negative dual variable(s) as small as -1.0482085035e-12.
Allowing negative dual variable(s) as small as -1.06272260957e-12.
Allowing negative dual variable(s) as small as -1.06180710925e-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 -1.48263476149e-12.
Allowing negative dual variable(s) as small as -1.14737863308e-13.
Allowing negative dual variable(s) as small as -6.26495383349e-15.
Allowing negative dual variable(s) as small as -1.6124645022e-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 -1.49485302033e-14.
Allowing negative dual variable(s) as small as -1.08187436509e-12.
Solving took 4 GP solves and 1.74 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 5.27 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -8.57045337477e-13.
Allowing negative dual variable(s) as small as -7.72417720063e-13.
Allowing negative dual variable(s) as small as -7.3815085988e-13.
Allowing negative dual variable(s) as small as -7.41276831584e-13.
Allowing negative dual variable(s) as small as -7.41431221973e-13.
Allowing negative dual variable(s) as small as -1.51903056106e-12.
Allowing negative dual variable(s) as small as -1.0468683212e-12.
Allowing negative dual variable(s) as small as -1.06121979693e-12.
Allowing negative dual variable(s) as small as -1.06332423335e-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 -1.48093061252e-12.
Allowing negative dual variable(s) as small as -1.14652970278e-13.
Allowing negative dual variable(s) as small as -5.35010404035e-15.
Allowing negative dual variable(s) as small as -1.62330327132e-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 -1.47645186482e-14.
Allowing negative dual variable(s) as small as -1.08032108788e-12.
Solving took 4 GP solves and 7.34 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 21.6 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Passed

Standard Output

Standard Error
