Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.0287465164222667e-14.
Allowing negative dual variable(s) as small as -7.645663616107079e-14.
Allowing negative dual variable(s) as small as -1.532940441251185e-13.
Allowing negative dual variable(s) as small as -1.4737993811464456e-13.
Solving took 4 GP solves and 2.87 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.290429552773368e-14.
Allowing negative dual variable(s) as small as -7.58945857548543e-14.
Allowing negative dual variable(s) as small as -1.4996944658340894e-13.
Allowing negative dual variable(s) as small as -1.5066290229293067e-13.
Solving took 4 GP solves and 3.35 seconds.
Allowing negative dual variable(s) as small as -5.182850676410666e-13.
Allowing negative dual variable(s) as small as -1.4289038702264278e-12.
Allowing negative dual variable(s) as small as -4.442921724967519e-13.
Allowing negative dual variable(s) as small as -4.446720769379908e-13.
Allowing negative dual variable(s) as small as -1.2982647725964802e-12.
Allowing negative dual variable(s) as small as -1.090722455930615e-12.
Allowing negative dual variable(s) as small as -1.0906960013976064e-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 -2.4751229902210544e-14.
Allowing negative dual variable(s) as small as -5.696157856516898e-12.
Allowing negative dual variable(s) as small as -2.087895314338984e-11.
Allowing negative dual variable(s) as small as -2.0880859124619304e-11.
Solving took 4 GP solves and 3.92 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.33 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.168695332846696e-13.
Allowing negative dual variable(s) as small as -1.4310445189957832e-12.
Allowing negative dual variable(s) as small as -4.44510747654725e-13.
Allowing negative dual variable(s) as small as -4.4492361184200746e-13.
Allowing negative dual variable(s) as small as -1.296279056317573e-12.
Allowing negative dual variable(s) as small as -1.0918584829669453e-12.
Allowing negative dual variable(s) as small as -1.0902799930240237e-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 -2.5014716758750295e-14.
Allowing negative dual variable(s) as small as -5.696082176081824e-12.
Allowing negative dual variable(s) as small as -2.0879049040357312e-11.
Allowing negative dual variable(s) as small as -2.0880787758943594e-11.
Solving took 4 GP solves and 3.26 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 3.12 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417

Passed

Standard Output

Standard Error