Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.97846947159e-13.
Allowing negative dual variable(s) as small as -4.11660722871e-13.
Solving took 4 GP solves and 2.32 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.17897748456e-13.
Allowing negative dual variable(s) as small as -3.33167087668e-13.
Allowing negative dual variable(s) as small as -7.27716498172e-15.
Solving took 4 GP solves and 2.64 seconds.
Allowing negative dual variable(s) as small as -2.3716584252e-12.
Allowing negative dual variable(s) as small as -2.70509743078e-13.
Allowing negative dual variable(s) as small as -1.09799842829e-12.
Allowing negative dual variable(s) as small as -1.10472655329e-12.
Allowing negative dual variable(s) as small as -1.09741588646e-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 = 21.754
speed at top of climb [m/s] = 26.532
design loiter speed [m/s] = 25.052
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 -2.20894851889e-12.
Allowing negative dual variable(s) as small as -7.03135466518e-14.
Allowing negative dual variable(s) as small as -1.18802970933e-13.
Allowing negative dual variable(s) as small as -1.17927260838e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.190
optimum loiter speed for min power, end of loiter [m/s] = 17.170
optimum cruise speed, inbound [m/s] = 35.882
optimum cruise speed, outbound [m/s] = 25.488
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.87881163379e-14.
Allowing negative dual variable(s) as small as -2.06154676491e-12.
Allowing negative dual variable(s) as small as -2.07726796757e-12.
Solving took 4 GP solves and 1.8 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.18123261708e-12.
Solving took 4 GP solves and 1.51 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -2.37164107797e-12.
Allowing negative dual variable(s) as small as -2.75113699183e-13.
Allowing negative dual variable(s) as small as -1.09698047087e-12.
Allowing negative dual variable(s) as small as -1.10510992718e-12.
Allowing negative dual variable(s) as small as -1.097004757e-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 = 21.754
speed at top of climb [m/s] = 26.532
design loiter speed [m/s] = 25.052
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 -2.21158876802e-12.
Allowing negative dual variable(s) as small as -7.08610687489e-14.
Allowing negative dual variable(s) as small as -1.17856354016e-13.
Allowing negative dual variable(s) as small as -1.19020461889e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.190
optimum loiter speed for min power, end of loiter [m/s] = 17.170
optimum cruise speed, inbound [m/s] = 35.882
optimum cruise speed, outbound [m/s] = 25.488
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.01352479892e-13.
Allowing negative dual variable(s) as small as -2.05827014665e-12.
Allowing negative dual variable(s) as small as -2.07707858577e-12.
Solving took 4 GP solves and 1.93 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.18343137909e-12.
Solving took 4 GP solves and 1.52 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Passed

Standard Output

Standard Error
