Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.25188488048e-13.
Allowing negative dual variable(s) as small as -4.65925041604e-14.
Solving took 4 GP solves and 9.86 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.14214193658e-13.
Allowing negative dual variable(s) as small as -4.52160010822e-14.
Allowing negative dual variable(s) as small as -5.94663207565e-15.
Solving took 4 GP solves and 3.08 seconds.
Allowing negative dual variable(s) as small as -2.37209037135e-12.
Allowing negative dual variable(s) as small as -2.67243692453e-13.
Allowing negative dual variable(s) as small as -1.09721910377e-12.
Allowing negative dual variable(s) as small as -1.1050215647e-12.
Allowing negative dual variable(s) as small as -1.097127055e-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 -2.21194655474e-12.
Allowing negative dual variable(s) as small as -7.06699239059e-14.
Allowing negative dual variable(s) as small as -1.1823734266e-13.
Allowing negative dual variable(s) as small as -1.19118365345e-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 -1.00339934378e-13.
Allowing negative dual variable(s) as small as -2.06184386781e-12.
Allowing negative dual variable(s) as small as -2.07884884377e-12.
Solving took 4 GP solves and 7.07 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.18214421427e-12.
Solving took 4 GP solves and 1.52 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -2.3698994156e-12.
Allowing negative dual variable(s) as small as -2.75504445646e-13.
Allowing negative dual variable(s) as small as -1.09721628484e-12.
Allowing negative dual variable(s) as small as -1.10531354035e-12.
Allowing negative dual variable(s) as small as -1.09697873615e-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 -2.21297372788e-12.
Allowing negative dual variable(s) as small as -7.01366048572e-14.
Allowing negative dual variable(s) as small as -1.18231379548e-13.
Allowing negative dual variable(s) as small as -1.18584287355e-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 -1.03291629053e-13.
Allowing negative dual variable(s) as small as -2.06006557989e-12.
Allowing negative dual variable(s) as small as -2.07782246906e-12.
Solving took 4 GP solves and 1.77 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.18306535244e-12.
Solving took 4 GP solves and 1.3 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Passed

Standard Output

Standard Error
