Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.02647878717e-14.
Allowing negative dual variable(s) as small as -8.19548422182e-14.
Allowing negative dual variable(s) as small as -1.50855022918e-13.
Allowing negative dual variable(s) as small as -1.50150291506e-13.
Solving took 4 GP solves and 5.04 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.08146952136e-14.
Allowing negative dual variable(s) as small as -8.06390544617e-14.
Allowing negative dual variable(s) as small as -1.50461240689e-13.
Allowing negative dual variable(s) as small as -1.47943289563e-13.
Solving took 4 GP solves and 4.31 seconds.
Allowing negative dual variable(s) as small as -5.23421583853e-13.
Allowing negative dual variable(s) as small as -5.12397416164e-13.
Allowing negative dual variable(s) as small as -5.1486592767e-13.
Allowing negative dual variable(s) as small as -5.1344345442e-13.
Allowing negative dual variable(s) as small as -2.38300698618e-13.
Allowing negative dual variable(s) as small as -1.79716267909e-14.
Allowing negative dual variable(s) as small as -1.25912680889e-12.
Allowing negative dual variable(s) as small as -1.25879829563e-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 -1.65952321329e-14.
Allowing negative dual variable(s) as small as -1.13315173217e-13.
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 -5.43412902981e-11.
Allowing negative dual variable(s) as small as -6.44965437593e-12.
Allowing negative dual variable(s) as small as -1.93392380738e-11.
Allowing negative dual variable(s) as small as -1.93546055288e-11.
Solving took 4 GP solves and 3.36 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.61 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.2261146799e-13.
Allowing negative dual variable(s) as small as -5.11167497219e-13.
Allowing negative dual variable(s) as small as -5.1649309829e-13.
Allowing negative dual variable(s) as small as -5.15034195847e-13.
Allowing negative dual variable(s) as small as -2.38063908864e-13.
Allowing negative dual variable(s) as small as -1.84875986048e-14.
Allowing negative dual variable(s) as small as -1.26061845424e-12.
Allowing negative dual variable(s) as small as -1.26000468739e-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 -1.93447688424e-14.
Allowing negative dual variable(s) as small as -1.13559986067e-13.
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 -5.43412106269e-11.
Allowing negative dual variable(s) as small as -6.44954351605e-12.
Allowing negative dual variable(s) as small as -1.93392457076e-11.
Allowing negative dual variable(s) as small as -1.93545822101e-11.
Solving took 4 GP solves and 2.28 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 5.3 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Passed

Standard Output

Standard Error
