Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.45265221863e-13.
Allowing negative dual variable(s) as small as -3.44239827615e-13.
Allowing negative dual variable(s) as small as -5.49633255575e-13.
Allowing negative dual variable(s) as small as -5.19752643702e-13.
Solving took 4 GP solves and 2.81 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 1155331.2270 but bound is 1000000.0000
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.41328700615e-13.
Allowing negative dual variable(s) as small as -3.54953479803e-13.
Allowing negative dual variable(s) as small as -5.25061331219e-13.
Allowing negative dual variable(s) as small as -5.29608908811e-13.
Solving took 4 GP solves and 2.71 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 1155331.2270 but bound is 1000000.0000
Allowing negative dual variable(s) as small as -8.5674262823e-13.
Allowing negative dual variable(s) as small as -7.72795889781e-13.
Allowing negative dual variable(s) as small as -7.38339077377e-13.
Allowing negative dual variable(s) as small as -7.41113767577e-13.
Allowing negative dual variable(s) as small as -7.41662807557e-13.
Allowing negative dual variable(s) as small as -1.51612229715e-12.
Allowing negative dual variable(s) as small as -1.04702249475e-12.
Allowing negative dual variable(s) as small as -1.062351704e-12.
Allowing negative dual variable(s) as small as -1.06360059648e-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 = 21.769
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 -1.48306779184e-12.
Allowing negative dual variable(s) as small as -1.15011190675e-13.
Allowing negative dual variable(s) as small as -5.73868209897e-15.
Allowing negative dual variable(s) as small as -1.60377895859e-13.
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 -1.4712391076e-14.
Allowing negative dual variable(s) as small as -1.08237565788e-12.
Solving took 4 GP solves and 2.47 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.
Solving took 4 GP solves and 1.54 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -8.56896151258e-13.
Allowing negative dual variable(s) as small as -7.72010060046e-13.
Allowing negative dual variable(s) as small as -7.38428415636e-13.
Allowing negative dual variable(s) as small as -7.41302852436e-13.
Allowing negative dual variable(s) as small as -7.41290709372e-13.
Allowing negative dual variable(s) as small as -1.51887508647e-12.
Allowing negative dual variable(s) as small as -1.048465351e-12.
Allowing negative dual variable(s) as small as -1.06163211902e-12.
Allowing negative dual variable(s) as small as -1.06277660283e-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 = 21.769
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 -1.47982169053e-12.
Allowing negative dual variable(s) as small as -1.14257128064e-13.
Allowing negative dual variable(s) as small as -5.85935380076e-15.
Allowing negative dual variable(s) as small as -1.61002938412e-13.
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 -1.52856422224e-14.
Allowing negative dual variable(s) as small as -1.08202938813e-12.
Solving took 4 GP solves and 2.52 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.
Solving took 4 GP solves and 1.72 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Passed

Standard Output

Standard Error
