Beginning signomial solve.
Allowing negative dual variable(s) as small as -6.19153296341e-12.
Allowing negative dual variable(s) as small as -5.02092985244e-12.
Allowing negative dual variable(s) as small as -4.77265883064e-12.
Allowing negative dual variable(s) as small as -1.95801153069e-11.
Solving took 4 GP solves and 1.8 seconds.
Warning: Variable [Re_Mission/Cruise/FlightSegment.1/AircraftPerf.1/TailAero.3_(0,)] could cause inaccurate result because it is above upper bound. Solution is 1155331.2266 but bound is 1000000.0000
Beginning signomial solve.
Allowing negative dual variable(s) as small as -6.16808383883e-12.
Allowing negative dual variable(s) as small as -4.99635922913e-12.
Allowing negative dual variable(s) as small as -4.75796268704e-12.
Allowing negative dual variable(s) as small as -1.01929246293e-11.
Solving took 4 GP solves and 1.73 seconds.
Warning: Variable [Re_Mission/Cruise/FlightSegment.1/AircraftPerf.1/TailAero.3_(0,)] could cause inaccurate result because it is above upper bound. Solution is 1155331.2268 but bound is 1000000.0000
Allowing negative dual variable(s) as small as -1.61003085863e-11.
Allowing negative dual variable(s) as small as -6.11773132153e-12.
Allowing negative dual variable(s) as small as -1.16452333887e-11.
Allowing negative dual variable(s) as small as -6.61015686632e-12.
Allowing negative dual variable(s) as small as -6.58047227819e-12.
Allowing negative dual variable(s) as small as -1.10147349141e-11.
Allowing negative dual variable(s) as small as -1.16819991181e-11.
Allowing negative dual variable(s) as small as -1.10547237597e-11.
Allowing negative dual variable(s) as small as -1.11143070658e-11.
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 = 21.769
speed at top of climb [m/s] = 26.550
design loiter speed [m/s] = 25.056
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 -1.79889200324e-11.
Allowing negative dual variable(s) as small as -6.27875052298e-12.
Allowing negative dual variable(s) as small as -1.04082182326e-11.
Allowing negative dual variable(s) as small as -1.04277582662e-11.
optimum loiter speed for min power, start of loiter [m/s] = 25.207
optimum loiter speed for min power, end of loiter [m/s] = 17.178
optimum cruise speed, inbound [m/s] = 36.034
optimum cruise speed, outbound [m/s] = 25.521
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.91658113477e-12.
Allowing negative dual variable(s) as small as -9.38317728743e-14.
Allowing negative dual variable(s) as small as -8.83162019536e-14.
Allowing negative dual variable(s) as small as -9.07574473635e-14.
Solving took 4 GP solves and 2.01 seconds.
Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1078212.3036 but bound is 1000000.0000
Max Speed [m/s]: 74.35
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.90950524762e-11.
Allowing negative dual variable(s) as small as -8.93246110759e-11.
Allowing negative dual variable(s) as small as -8.98761811502e-11.
Allowing negative dual variable(s) as small as -8.47859647074e-11.
Solving took 4 GP solves and 4.05 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -1.61052698955e-11.
Allowing negative dual variable(s) as small as -6.0989824302e-12.
Allowing negative dual variable(s) as small as -1.16477105738e-11.
Allowing negative dual variable(s) as small as -6.62146726338e-12.
Allowing negative dual variable(s) as small as -6.61683208225e-12.
Allowing negative dual variable(s) as small as -1.10092885329e-11.
Allowing negative dual variable(s) as small as -1.16818949262e-11.
Allowing negative dual variable(s) as small as -1.10534880944e-11.
Allowing negative dual variable(s) as small as -1.11131560768e-11.
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 = 21.769
speed at top of climb [m/s] = 26.550
design loiter speed [m/s] = 25.056
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 -1.7985868437e-11.
Allowing negative dual variable(s) as small as -6.27540315719e-12.
Allowing negative dual variable(s) as small as -1.04080099574e-11.
Allowing negative dual variable(s) as small as -1.04264325038e-11.
optimum loiter speed for min power, start of loiter [m/s] = 25.207
optimum loiter speed for min power, end of loiter [m/s] = 17.178
optimum cruise speed, inbound [m/s] = 36.034
optimum cruise speed, outbound [m/s] = 25.521
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.91675417343e-12.
Allowing negative dual variable(s) as small as -2.44064135732e-13.
Allowing negative dual variable(s) as small as -8.8296649998e-14.
Allowing negative dual variable(s) as small as -9.08631865097e-14.
Solving took 4 GP solves and 1.98 seconds.
Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1078212.3036 but bound is 1000000.0000
Max Speed [m/s]: 74.35
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.91045140918e-11.
Allowing negative dual variable(s) as small as -8.92982710346e-11.
Allowing negative dual variable(s) as small as -8.98768776417e-11.
Allowing negative dual variable(s) as small as -8.47945351087e-11.
Solving took 4 GP solves and 5.04 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Passed

Standard Output

Standard Error
