Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.13424027115e-13.
Allowing negative dual variable(s) as small as -7.00881193361e-13.
Solving took 4 GP solves and 1.21 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.13424027115e-13.
Allowing negative dual variable(s) as small as -7.00881193361e-13.
Solving took 4 GP solves and 1.01 seconds.
Allowing negative dual variable(s) as small as -2.37041896528e-12.
Allowing negative dual variable(s) as small as -2.71481838746e-13.
Allowing negative dual variable(s) as small as -1.0965677151e-12.
Allowing negative dual variable(s) as small as -1.1049180234e-12.
Allowing negative dual variable(s) as small as -1.09640085639e-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 -2.21014916438e-12.
Allowing negative dual variable(s) as small as -7.06454209368e-14.
Allowing negative dual variable(s) as small as -1.18886996602e-13.
Allowing negative dual variable(s) as small as -1.17911214646e-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 -1.01295510627e-13.
Allowing negative dual variable(s) as small as -2.06011842559e-12.
Allowing negative dual variable(s) as small as -2.07832074122e-12.
Solving took 4 GP solves and 2.18 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.18209564201e-12.
Solving took 4 GP solves and 1.81 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -2.37041896528e-12.
Allowing negative dual variable(s) as small as -2.71481838746e-13.
Allowing negative dual variable(s) as small as -1.0965677151e-12.
Allowing negative dual variable(s) as small as -1.1049180234e-12.
Allowing negative dual variable(s) as small as -1.09640085639e-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 -2.21014916438e-12.
Allowing negative dual variable(s) as small as -7.06454209368e-14.
Allowing negative dual variable(s) as small as -1.18886996602e-13.
Allowing negative dual variable(s) as small as -1.17911214646e-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 -1.01295510627e-13.
Allowing negative dual variable(s) as small as -2.06011842559e-12.
Allowing negative dual variable(s) as small as -2.07832074122e-12.
Solving took 4 GP solves and 2.34 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.18209564201e-12.
Solving took 4 GP solves and 1.15 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Passed

Standard Output

Standard Error
