Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.32514658968e-13.
Allowing negative dual variable(s) as small as -3.42682479615e-13.
Solving took 4 GP solves and 2.46 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.33820472065e-13.
Allowing negative dual variable(s) as small as -3.18413264505e-13.
Solving took 4 GP solves and 6.36 seconds.
Allowing negative dual variable(s) as small as -2.36994278369e-12.
Allowing negative dual variable(s) as small as -2.68450626312e-13.
Allowing negative dual variable(s) as small as -1.09758990091e-12.
Allowing negative dual variable(s) as small as -1.10465738119e-12.
Allowing negative dual variable(s) as small as -1.09735343642e-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 -2.21244160145e-12.
Allowing negative dual variable(s) as small as -7.08772233612e-14.
Allowing negative dual variable(s) as small as -1.18566181179e-13.
Allowing negative dual variable(s) as small as -1.18234090053e-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 -9.99887672765e-14.
Allowing negative dual variable(s) as small as -2.06050409976e-12.
Allowing negative dual variable(s) as small as -2.07688040283e-12.
Solving took 4 GP solves and 16.1 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.17890375082e-12.
Solving took 4 GP solves and 37 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -2.37042503681e-12.
Allowing negative dual variable(s) as small as -2.76683190248e-13.
Allowing negative dual variable(s) as small as -1.0969452343e-12.
Allowing negative dual variable(s) as small as -1.10498730391e-12.
Allowing negative dual variable(s) as small as -1.09646666746e-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 -2.21166683058e-12.
Allowing negative dual variable(s) as small as -7.02426398297e-14.
Allowing negative dual variable(s) as small as -1.18809259306e-13.
Allowing negative dual variable(s) as small as -1.18833328594e-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 -1.01306470598e-13.
Allowing negative dual variable(s) as small as -2.06248089778e-12.
Allowing negative dual variable(s) as small as -2.07672399364e-12.
Solving took 4 GP solves and 12.8 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.18421807619e-12.
Solving took 4 GP solves and 8.34 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Passed

Standard Output

Standard Error
