Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.1059686153e-13.
Allowing negative dual variable(s) as small as -1.07221957008e-13.
Solving took 4 GP solves and 6.53 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.09034309359e-13.
Allowing negative dual variable(s) as small as -1.04471119255e-13.
Solving took 4 GP solves and 1.38 seconds.
Allowing negative dual variable(s) as small as -3.88091989101e-12.
Allowing negative dual variable(s) as small as -1.71243054459e-12.
Allowing negative dual variable(s) as small as -7.75130827579e-13.
Allowing negative dual variable(s) as small as -7.70415849172e-13.
Allowing negative dual variable(s) as small as -7.70459217259e-13.
Allowing negative dual variable(s) as small as -2.48689523835e-13.
Allowing negative dual variable(s) as small as -1.01719327406e-12.
Allowing negative dual variable(s) as small as -1.05813437439e-12.
Allowing negative dual variable(s) as small as -1.04753044346e-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 -2.59304296785e-13.
Allowing negative dual variable(s) as small as -1.46376617424e-13.
Allowing negative dual variable(s) as small as -1.47298622952e-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 -3.99829117213e-13.
Allowing negative dual variable(s) as small as -2.00462967759e-15.
Allowing negative dual variable(s) as small as -8.84573386596e-14.
Allowing negative dual variable(s) as small as -8.84710673167e-14.
Solving took 4 GP solves and 8.81 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 11.1 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -3.88134489826e-12.
Allowing negative dual variable(s) as small as -1.71271503924e-12.
Allowing negative dual variable(s) as small as -7.75615682791e-13.
Allowing negative dual variable(s) as small as -7.7031523521e-13.
Allowing negative dual variable(s) as small as -7.6966124446e-13.
Allowing negative dual variable(s) as small as -2.50795478135e-13.
Allowing negative dual variable(s) as small as -1.0170079839e-12.
Allowing negative dual variable(s) as small as -1.05705993004e-12.
Allowing negative dual variable(s) as small as -1.04718241457e-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 -2.58465341144e-13.
Allowing negative dual variable(s) as small as -1.48245348289e-13.
Allowing negative dual variable(s) as small as -1.47467866911e-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 -4.00317464317e-13.
Allowing negative dual variable(s) as small as -1.50511767263e-15.
Allowing negative dual variable(s) as small as -8.91792476352e-14.
Allowing negative dual variable(s) as small as -9.03500986842e-14.
Solving took 4 GP solves and 7.62 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 1.29 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Passed

Standard Output

Standard Error
