Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.339894771e-13.
Allowing negative dual variable(s) as small as -4.13777519193e-13.
Solving took 4 GP solves and 3.06 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.14771473575e-13.
Allowing negative dual variable(s) as small as -2.69759041494e-13.
Solving took 4 GP solves and 7.9 seconds.
Allowing negative dual variable(s) as small as -2.37151444316e-12.
Allowing negative dual variable(s) as small as -2.68444121099e-13.
Allowing negative dual variable(s) as small as -1.09756127797e-12.
Allowing negative dual variable(s) as small as -1.10499998908e-12.
Allowing negative dual variable(s) as small as -1.09763999105e-12.
MTOW [lbs] = 141.59
Zero fuel weight [lbs] = 53.63
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 = 21.754
speed at top of climb [m/s] = 26.532
design loiter speed [m/s] = 25.052
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -2.21186957639e-12.
Allowing negative dual variable(s) as small as -6.9988286e-14.
Allowing negative dual variable(s) as small as -1.1824764258e-13.
Allowing negative dual variable(s) as small as -1.18540160327e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.190
optimum loiter speed for min power, end of loiter [m/s] = 17.170
optimum cruise speed, inbound [m/s] = 35.882
optimum cruise speed, outbound [m/s] = 25.488
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.02021648997e-13.
Allowing negative dual variable(s) as small as -2.06069445712e-12.
Allowing negative dual variable(s) as small as -2.07997781443e-12.
Solving took 4 GP solves and 40.6 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.18472808489e-12.
Solving took 4 GP solves and 2.42 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -2.372497164e-12.
Allowing negative dual variable(s) as small as -2.66445285974e-13.
Allowing negative dual variable(s) as small as -1.0965580657e-12.
Allowing negative dual variable(s) as small as -1.10482283044e-12.
Allowing negative dual variable(s) as small as -1.09695564264e-12.
MTOW [lbs] = 141.59
Zero fuel weight [lbs] = 53.63
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 = 21.754
speed at top of climb [m/s] = 26.532
design loiter speed [m/s] = 25.052
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -2.21182490726e-12.
Allowing negative dual variable(s) as small as -7.02515302875e-14.
Allowing negative dual variable(s) as small as -1.18109840484e-13.
Allowing negative dual variable(s) as small as -1.18488552303e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.190
optimum loiter speed for min power, end of loiter [m/s] = 17.170
optimum cruise speed, inbound [m/s] = 35.882
optimum cruise speed, outbound [m/s] = 25.488
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.01792132979e-13.
Allowing negative dual variable(s) as small as -2.06330061572e-12.
Allowing negative dual variable(s) as small as -2.07714561859e-12.
Solving took 4 GP solves and 471 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.17995239116e-12.
Solving took 4 GP solves and 274 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Passed

Standard Output

Standard Error
