Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.962176503031657e-14.
Allowing negative dual variable(s) as small as -7.66951606390176e-14.
Allowing negative dual variable(s) as small as -1.5117204363312986e-13.
Allowing negative dual variable(s) as small as -1.4655160765486563e-13.
Solving took 4 GP solves and 3.7 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.1811853418737286e-14.
Allowing negative dual variable(s) as small as -7.373095189944223e-14.
Allowing negative dual variable(s) as small as -1.4907693135501887e-13.
Allowing negative dual variable(s) as small as -1.4826855021521368e-13.
Solving took 4 GP solves and 3.28 seconds.
Allowing negative dual variable(s) as small as -5.18106391123041e-13.
Allowing negative dual variable(s) as small as -1.431054927336639e-12.
Allowing negative dual variable(s) as small as -4.4566607348972553e-13.
Allowing negative dual variable(s) as small as -4.4441533786354626e-13.
Allowing negative dual variable(s) as small as -1.2968578034372458e-12.
Allowing negative dual variable(s) as small as -1.092011897574352e-12.
Allowing negative dual variable(s) as small as -1.0902651394542606e-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 -2.479799088545931e-14.
Allowing negative dual variable(s) as small as -5.696020621668152e-12.
Allowing negative dual variable(s) as small as -2.0879005876378883e-11.
Allowing negative dual variable(s) as small as -2.088085500917738e-11.
Solving took 4 GP solves and 2.99 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 -5.17207804362485e-13.
Allowing negative dual variable(s) as small as -1.429646331874146e-12.
Allowing negative dual variable(s) as small as -4.4589679171203045e-13.
Allowing negative dual variable(s) as small as -4.4656292552680554e-13.
Allowing negative dual variable(s) as small as -1.2979047090549978e-12.
Allowing negative dual variable(s) as small as -1.090401857348211e-12.
Allowing negative dual variable(s) as small as -1.0910458734386674e-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 -1.3717325886286602e-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 -2.404943557683957e-14.
Allowing negative dual variable(s) as small as -5.696003693899989e-12.
Allowing negative dual variable(s) as small as -2.087902899352267e-11.
Allowing negative dual variable(s) as small as -2.0880681265435133e-11.
Solving took 4 GP solves and 3.42 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.94 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Passed

Standard Output

Standard Error
