Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.54016901799e-13.
Allowing negative dual variable(s) as small as -3.06001751715e-13.
Allowing negative dual variable(s) as small as -5.60026851282e-13.
Allowing negative dual variable(s) as small as -5.38478549944e-13.
Solving took 4 GP solves and 1.93 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 -5.40739328314e-13.
Allowing negative dual variable(s) as small as -3.07799358917e-13.
Allowing negative dual variable(s) as small as -5.25776037291e-13.
Allowing negative dual variable(s) as small as -5.2672840048e-13.
Solving took 4 GP solves and 4.37 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 -8.57218809824e-13.
Allowing negative dual variable(s) as small as -7.72338790145e-13.
Allowing negative dual variable(s) as small as -7.38617500495e-13.
Allowing negative dual variable(s) as small as -7.41058256426e-13.
Allowing negative dual variable(s) as small as -7.41043511276e-13.
Allowing negative dual variable(s) as small as -1.51862116632e-12.
Allowing negative dual variable(s) as small as -1.04697533195e-12.
Allowing negative dual variable(s) as small as -1.06079283812e-12.
Allowing negative dual variable(s) as small as -1.06328379261e-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 -1.47987698484e-12.
Allowing negative dual variable(s) as small as -1.14288895188e-13.
Allowing negative dual variable(s) as small as -4.70923213619e-15.
Allowing negative dual variable(s) as small as -1.60940922048e-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 -1.50771695205e-14.
Allowing negative dual variable(s) as small as -1.08199474208e-12.
Solving took 4 GP solves and 8.05 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 1.94 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -8.56788598402e-13.
Allowing negative dual variable(s) as small as -7.72456751341e-13.
Allowing negative dual variable(s) as small as -7.38275759971e-13.
Allowing negative dual variable(s) as small as -7.41956843187e-13.
Allowing negative dual variable(s) as small as -7.4111029813e-13.
Allowing negative dual variable(s) as small as -1.51656400112e-12.
Allowing negative dual variable(s) as small as -1.04775292175e-12.
Allowing negative dual variable(s) as small as -1.0626691584e-12.
Allowing negative dual variable(s) as small as -1.06422954217e-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 -1.47789289487e-12.
Allowing negative dual variable(s) as small as -1.13548276684e-13.
Allowing negative dual variable(s) as small as -5.89090408398e-15.
Allowing negative dual variable(s) as small as -1.61156136179e-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 -1.46934465488e-14.
Allowing negative dual variable(s) as small as -1.08182824274e-12.
Solving took 4 GP solves and 20.4 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 1.48 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Passed

Standard Output

Standard Error
