Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.06039742959e-13.
Allowing negative dual variable(s) as small as -3.4797989143e-13.
Solving took 4 GP solves and 1.33 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.02642287031e-13.
Allowing negative dual variable(s) as small as -7.19425821e-13.
Allowing negative dual variable(s) as small as -2.15799600412e-15.
Solving took 4 GP solves and 0.991 seconds.
Allowing negative dual variable(s) as small as -2.37317630825e-12.
Allowing negative dual variable(s) as small as -2.68050122029e-13.
Allowing negative dual variable(s) as small as -1.09786008409e-12.
Allowing negative dual variable(s) as small as -1.10468188416e-12.
Allowing negative dual variable(s) as small as -1.09733121027e-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 -2.2108775314e-12.
Allowing negative dual variable(s) as small as -7.0433459412e-14.
Allowing negative dual variable(s) as small as -1.18613452393e-13.
Allowing negative dual variable(s) as small as -1.1841233289e-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 -1.00560808913e-13.
Allowing negative dual variable(s) as small as -2.0609598417e-12.
Allowing negative dual variable(s) as small as -2.07920884293e-12.
Solving took 4 GP solves and 1.65 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.18376878281e-12.
Solving took 4 GP solves and 1.45 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -2.37238353962e-12.
Allowing negative dual variable(s) as small as -2.71249819481e-13.
Allowing negative dual variable(s) as small as -1.09784035161e-12.
Allowing negative dual variable(s) as small as -1.10505745179e-12.
Allowing negative dual variable(s) as small as -1.0972166101e-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 -2.21175421727e-12.
Allowing negative dual variable(s) as small as -6.94417396849e-14.
Allowing negative dual variable(s) as small as -1.18569433785e-13.
Allowing negative dual variable(s) as small as -1.18798634124e-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 -1.03085392571e-13.
Allowing negative dual variable(s) as small as -2.05932557157e-12.
Allowing negative dual variable(s) as small as -2.07879709863e-12.
Solving took 4 GP solves and 90.5 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.18317464002e-12.
Solving took 4 GP solves and 46.8 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Passed

Standard Output

Standard Error
