Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.59014206453e-13.
Allowing negative dual variable(s) as small as -3.13012202963e-13.
Allowing negative dual variable(s) as small as -5.22572870393e-13.
Allowing negative dual variable(s) as small as -5.35191248957e-13.
Solving took 4 GP solves and 2.02 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 -5.60852579656e-13.
Allowing negative dual variable(s) as small as -3.27689264612e-13.
Allowing negative dual variable(s) as small as -5.23758553889e-13.
Allowing negative dual variable(s) as small as -5.52411848903e-13.
Solving took 4 GP solves and 5.08 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 -8.57496365581e-13.
Allowing negative dual variable(s) as small as -7.72158378903e-13.
Allowing negative dual variable(s) as small as -7.38416272572e-13.
Allowing negative dual variable(s) as small as -7.41490202572e-13.
Allowing negative dual variable(s) as small as -7.41753013178e-13.
Allowing negative dual variable(s) as small as -1.51567864162e-12.
Allowing negative dual variable(s) as small as -1.04792303307e-12.
Allowing negative dual variable(s) as small as -1.06308614255e-12.
Allowing negative dual variable(s) as small as -1.06273366843e-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 -1.48311788198e-12.
Allowing negative dual variable(s) as small as -1.1383569868e-13.
Allowing negative dual variable(s) as small as -5.68241200621e-15.
Allowing negative dual variable(s) as small as -1.61532788014e-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 -1.56079399529e-14.
Allowing negative dual variable(s) as small as -1.08085512984e-12.
Solving took 4 GP solves and 1.58 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 5.22 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -8.57117328501e-13.
Allowing negative dual variable(s) as small as -7.72021335749e-13.
Allowing negative dual variable(s) as small as -7.38847351356e-13.
Allowing negative dual variable(s) as small as -7.41135451621e-13.
Allowing negative dual variable(s) as small as -7.40890855611e-13.
Allowing negative dual variable(s) as small as -1.52232198201e-12.
Allowing negative dual variable(s) as small as -1.0479167447e-12.
Allowing negative dual variable(s) as small as -1.06327652846e-12.
Allowing negative dual variable(s) as small as -1.06280099738e-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 -1.48015432376e-12.
Allowing negative dual variable(s) as small as -1.15144113862e-13.
Allowing negative dual variable(s) as small as -5.51815537708e-15.
Allowing negative dual variable(s) as small as -1.6074750038e-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 -1.50204020076e-14.
Allowing negative dual variable(s) as small as -1.08040287627e-12.
Solving took 4 GP solves and 7.67 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 22 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Passed

Standard Output

Standard Error
