Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.023021928951543e-14.
Allowing negative dual variable(s) as small as -7.357742887181828e-14.
Allowing negative dual variable(s) as small as -1.5164215369511957e-13.
Allowing negative dual variable(s) as small as -1.4890085692220723e-13.
Solving took 4 GP solves and 2.79 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.1377305188005096e-14.
Allowing negative dual variable(s) as small as -7.40627177642228e-14.
Allowing negative dual variable(s) as small as -1.5064251929208794e-13.
Allowing negative dual variable(s) as small as -1.4909991644107556e-13.
Solving took 4 GP solves and 2.92 seconds.
Allowing negative dual variable(s) as small as -5.188297708125233e-13.
Allowing negative dual variable(s) as small as -1.43054144918775e-12.
Allowing negative dual variable(s) as small as -4.451369828295526e-13.
Allowing negative dual variable(s) as small as -4.446738116614668e-13.
Allowing negative dual variable(s) as small as -1.2966744648498785e-12.
Allowing negative dual variable(s) as small as -1.091298275704422e-12.
Allowing negative dual variable(s) as small as -1.0907411042079818e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
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 = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.41020072061065e-14.
Allowing negative dual variable(s) as small as -5.6961012152384265e-12.
Allowing negative dual variable(s) as small as -2.0879096032395267e-11.
Allowing negative dual variable(s) as small as -2.088073862309172e-11.
Solving took 4 GP solves and 3.21 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.29 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.184741524999481e-13.
Allowing negative dual variable(s) as small as -1.429037443934078e-12.
Allowing negative dual variable(s) as small as -4.4269622689885324e-13.
Allowing negative dual variable(s) as small as -4.4383420549909403e-13.
Allowing negative dual variable(s) as small as -1.2967866797747307e-12.
Allowing negative dual variable(s) as small as -1.090790543827047e-12.
Allowing negative dual variable(s) as small as -1.0914456187796628e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
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 = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.436208030811058e-14.
Allowing negative dual variable(s) as small as -5.696152269964034e-12.
Allowing negative dual variable(s) as small as -2.0879152623222338e-11.
Allowing negative dual variable(s) as small as -2.0880872586063948e-11.
Solving took 4 GP solves and 2.57 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.94 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Passed

Standard Output

Standard Error
