Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.04631581177e-13.
Allowing negative dual variable(s) as small as -1.02650526967e-13.
Allowing negative dual variable(s) as small as -9.6147048656e-16.
Allowing negative dual variable(s) as small as -4.90059381963e-16.
Solving took 4 GP solves and 6.55 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.21270615078e-13.
Allowing negative dual variable(s) as small as -1.00590109159e-13.
Allowing negative dual variable(s) as small as -1.22254636969e-15.
Allowing negative dual variable(s) as small as -4.07660016855e-16.
Solving took 4 GP solves and 1.72 seconds.
Allowing negative dual variable(s) as small as -3.88233889481e-12.
Allowing negative dual variable(s) as small as -1.71259881276e-12.
Allowing negative dual variable(s) as small as -7.75203685965e-13.
Allowing negative dual variable(s) as small as -7.69979566217e-13.
Allowing negative dual variable(s) as small as -7.70293551167e-13.
Allowing negative dual variable(s) as small as -2.49512866965e-13.
Allowing negative dual variable(s) as small as -1.01795601028e-12.
Allowing negative dual variable(s) as small as -1.05584421414e-12.
Allowing negative dual variable(s) as small as -1.04741356647e-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 -2.59410114917e-13.
Allowing negative dual variable(s) as small as -1.47014670403e-13.
Allowing negative dual variable(s) as small as -1.48594678229e-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 -4.00698349411e-13.
Allowing negative dual variable(s) as small as -1.02669784685e-15.
Allowing negative dual variable(s) as small as -8.98690415684e-14.
Allowing negative dual variable(s) as small as -8.69332665072e-14.
Solving took 4 GP solves and 18.3 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 1.09 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -3.8824637949e-12.
Allowing negative dual variable(s) as small as -1.71187543307e-12.
Allowing negative dual variable(s) as small as -7.75911453144e-13.
Allowing negative dual variable(s) as small as -7.70384624149e-13.
Allowing negative dual variable(s) as small as -7.70837386976e-13.
Allowing negative dual variable(s) as small as -2.5259959055e-13.
Allowing negative dual variable(s) as small as -1.01674560698e-12.
Allowing negative dual variable(s) as small as -1.05649029022e-12.
Allowing negative dual variable(s) as small as -1.04833904144e-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 -2.60222616025e-13.
Allowing negative dual variable(s) as small as -1.47553085202e-13.
Allowing negative dual variable(s) as small as -1.47351748858e-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 -4.00198322992e-13.
Allowing negative dual variable(s) as small as -3.22182264024e-15.
Allowing negative dual variable(s) as small as -8.75203212201e-14.
Allowing negative dual variable(s) as small as -8.98626579575e-14.
Solving took 4 GP solves and 1.72 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 1.08 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Passed

Standard Output

Standard Error
