Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.3382515422e-13.
Allowing negative dual variable(s) as small as -3.73467749781e-13.
Allowing negative dual variable(s) as small as -5.25572640964e-13.
Allowing negative dual variable(s) as small as -5.08453522341e-13.
Solving took 4 GP solves and 1.89 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 -5.46485166147e-13.
Allowing negative dual variable(s) as small as -3.27810695255e-13.
Allowing negative dual variable(s) as small as -5.27263128991e-13.
Allowing negative dual variable(s) as small as -5.2989774027e-13.
Solving took 4 GP solves and 5.94 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 -8.57184115355e-13.
Allowing negative dual variable(s) as small as -7.72739511268e-13.
Allowing negative dual variable(s) as small as -7.38267953715e-13.
Allowing negative dual variable(s) as small as -7.41836279905e-13.
Allowing negative dual variable(s) as small as -7.41331475373e-13.
Allowing negative dual variable(s) as small as -1.51295794469e-12.
Allowing negative dual variable(s) as small as -1.04653417009e-12.
Allowing negative dual variable(s) as small as -1.0618915686e-12.
Allowing negative dual variable(s) as small as -1.06209355547e-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 -1.48312200195e-12.
Allowing negative dual variable(s) as small as -1.13212607691e-13.
Allowing negative dual variable(s) as small as -7.06661291983e-15.
Allowing negative dual variable(s) as small as -1.61414284716e-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 -1.53124279452e-14.
Allowing negative dual variable(s) as small as -1.08146393324e-12.
Solving took 4 GP solves and 6.44 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 2 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -8.57374934937e-13.
Allowing negative dual variable(s) as small as -7.72183532394e-13.
Allowing negative dual variable(s) as small as -7.38631378283e-13.
Allowing negative dual variable(s) as small as -7.41119839109e-13.
Allowing negative dual variable(s) as small as -7.41510151892e-13.
Allowing negative dual variable(s) as small as -1.52053955364e-12.
Allowing negative dual variable(s) as small as -1.04665278181e-12.
Allowing negative dual variable(s) as small as -1.06274971462e-12.
Allowing negative dual variable(s) as small as -1.06256258132e-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 -1.47932035545e-12.
Allowing negative dual variable(s) as small as -1.14265368001e-13.
Allowing negative dual variable(s) as small as -6.80499493561e-15.
Allowing negative dual variable(s) as small as -1.6148595048e-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 -1.54569572829e-14.
Allowing negative dual variable(s) as small as -1.08245419975e-12.
Solving took 4 GP solves and 22.7 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 1.44 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Passed

Standard Output

Standard Error
