Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.45260451373e-13.
Allowing negative dual variable(s) as small as -3.36175965537e-13.
Allowing negative dual variable(s) as small as -5.35200356255e-13.
Allowing negative dual variable(s) as small as -5.46682924624e-13.
Solving took 4 GP solves and 2.68 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
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.5318380085e-13.
Allowing negative dual variable(s) as small as -3.38390340054e-13.
Allowing negative dual variable(s) as small as -5.19689759976e-13.
Allowing negative dual variable(s) as small as -5.18383946879e-13.
Solving took 4 GP solves and 2.82 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 -8.56763444912e-13.
Allowing negative dual variable(s) as small as -7.72212155331e-13.
Allowing negative dual variable(s) as small as -7.3831565861e-13.
Allowing negative dual variable(s) as small as -7.41360965673e-13.
Allowing negative dual variable(s) as small as -7.4105045017e-13.
Allowing negative dual variable(s) as small as -1.51570119303e-12.
Allowing negative dual variable(s) as small as -1.04603652129e-12.
Allowing negative dual variable(s) as small as -1.06180071246e-12.
Allowing negative dual variable(s) as small as -1.06151068838e-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 -1.48156313606e-12.
Allowing negative dual variable(s) as small as -1.14692218396e-13.
Allowing negative dual variable(s) as small as -5.78942276064e-15.
Allowing negative dual variable(s) as small as -1.60324661533e-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 -1.52081719537e-14.
Allowing negative dual variable(s) as small as -1.08186353882e-12.
Solving took 4 GP solves and 2.25 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 1.79 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -8.57044470115e-13.
Allowing negative dual variable(s) as small as -7.72596396581e-13.
Allowing negative dual variable(s) as small as -7.38653062327e-13.
Allowing negative dual variable(s) as small as -7.41704440921e-13.
Allowing negative dual variable(s) as small as -7.41368771928e-13.
Allowing negative dual variable(s) as small as -1.51864697033e-12.
Allowing negative dual variable(s) as small as -1.04785700516e-12.
Allowing negative dual variable(s) as small as -1.06259879368e-12.
Allowing negative dual variable(s) as small as -1.06234031988e-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 -1.47876481026e-12.
Allowing negative dual variable(s) as small as -1.14382244995e-13.
Allowing negative dual variable(s) as small as -6.34778687947e-15.
Allowing negative dual variable(s) as small as -1.62037592545e-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 -1.50828812754e-14.
Allowing negative dual variable(s) as small as -1.0815379208e-12.
Solving took 4 GP solves and 2.2 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 1.5 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Passed

Standard Output

Standard Error
