Beginning signomial solve.
Allowing negative dual variable(s) as small as -6.81468336622e-13.
Solving took 4 GP solves and 1.49 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -6.65017086537e-13.
Solving took 4 GP solves and 1.13 seconds.
Allowing negative dual variable(s) as small as -3.6009441956e-12.
Allowing negative dual variable(s) as small as -1.58866062666e-12.
Allowing negative dual variable(s) as small as -1.77649128047e-12.
Allowing negative dual variable(s) as small as -7.79497126568e-13.
Allowing negative dual variable(s) as small as -7.77777148242e-13.
Allowing negative dual variable(s) as small as -2.82132607207e-13.
Allowing negative dual variable(s) as small as -1.09972024976e-12.
Allowing negative dual variable(s) as small as -1.06865839962e-12.
Allowing negative dual variable(s) as small as -1.06237327963e-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 -2.27179603254e-12.
Allowing negative dual variable(s) as small as -7.25780113092e-14.
Allowing negative dual variable(s) as small as -1.21156014908e-13.
Allowing negative dual variable(s) as small as -1.21518897375e-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 -2.64165986016e-12.
Allowing negative dual variable(s) as small as -1.9767177444e-12.
Allowing negative dual variable(s) as small as -1.99621265973e-12.
Solving took 4 GP solves and 1.99 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.85110259654e-12.
Solving took 4 GP solves and 1.13 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -3.60190349769e-12.
Allowing negative dual variable(s) as small as -1.58822868052e-12.
Allowing negative dual variable(s) as small as -1.77697266623e-12.
Allowing negative dual variable(s) as small as -7.78179604088e-13.
Allowing negative dual variable(s) as small as -7.78687878067e-13.
Allowing negative dual variable(s) as small as -2.83235240817e-13.
Allowing negative dual variable(s) as small as -1.09832607419e-12.
Allowing negative dual variable(s) as small as -1.06871629602e-12.
Allowing negative dual variable(s) as small as -1.06208358081e-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 -2.27442587333e-12.
Allowing negative dual variable(s) as small as -7.1745452461e-14.
Allowing negative dual variable(s) as small as -1.20911418898e-13.
Allowing negative dual variable(s) as small as -1.20523599781e-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 -2.64236390452e-12.
Allowing negative dual variable(s) as small as -1.975059183e-12.
Allowing negative dual variable(s) as small as -1.99597647079e-12.
Solving took 4 GP solves and 1.73 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.84973563444e-12.
Solving took 4 GP solves and 1.33 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Passed

Standard Output

Standard Error
