Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.050126983263681e-14.
Allowing negative dual variable(s) as small as -7.590672881918614e-14.
Allowing negative dual variable(s) as small as -1.5105191403241847e-13.
Allowing negative dual variable(s) as small as -1.4975260614891184e-13.
Solving took 4 GP solves and 2.83 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.0065420559297635e-14.
Allowing negative dual variable(s) as small as -7.408396812680351e-14.
Allowing negative dual variable(s) as small as -1.5029123778820264e-13.
Allowing negative dual variable(s) as small as -1.49964242412981e-13.
Solving took 4 GP solves and 2.89 seconds.
Allowing negative dual variable(s) as small as -5.183093537697303e-13.
Allowing negative dual variable(s) as small as -1.4299846029519614e-12.
Allowing negative dual variable(s) as small as -4.4411002653177434e-13.
Allowing negative dual variable(s) as small as -4.4534341492319385e-13.
Allowing negative dual variable(s) as small as -1.296652889226646e-12.
Allowing negative dual variable(s) as small as -1.091077532142104e-12.
Allowing negative dual variable(s) as small as -1.0907750397359806e-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
Allowing negative dual variable(s) as small as -2.6935918773229872e-15.
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 -2.6323134905121117e-14.
Allowing negative dual variable(s) as small as -5.695990546995736e-12.
Allowing negative dual variable(s) as small as -2.0878980496915973e-11.
Allowing negative dual variable(s) as small as -2.0880920619396563e-11.
Solving took 4 GP solves and 3.02 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.81 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.155962462533026e-13.
Allowing negative dual variable(s) as small as -1.429564799870775e-12.
Allowing negative dual variable(s) as small as -4.45107492530461e-13.
Allowing negative dual variable(s) as small as -4.447033019605584e-13.
Allowing negative dual variable(s) as small as -1.296481043182307e-12.
Allowing negative dual variable(s) as small as -1.0922071623856167e-12.
Allowing negative dual variable(s) as small as -1.0929329273198785e-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
Allowing negative dual variable(s) as small as -1.7433970933566911e-16.
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 -2.4087889072699903e-14.
Allowing negative dual variable(s) as small as -5.695981004904887e-12.
Allowing negative dual variable(s) as small as -2.0878942246231564e-11.
Allowing negative dual variable(s) as small as -2.088071071287965e-11.
Solving took 4 GP solves and 2.77 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.71 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Passed

Standard Output

Standard Error
