Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.56775675911e-12.
Allowing negative dual variable(s) as small as -4.97715800865e-12.
Allowing negative dual variable(s) as small as -4.73643823815e-12.
Allowing negative dual variable(s) as small as -1.98190938487e-11.
Solving took 4 GP solves and 6.25 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 -1.16076618803e-11.
Allowing negative dual variable(s) as small as -5.00822560506e-12.
Allowing negative dual variable(s) as small as -4.78342105509e-12.
Allowing negative dual variable(s) as small as -1.96310814826e-11.
Solving took 4 GP solves and 1.77 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
Allowing negative dual variable(s) as small as -1.61165941703e-11.
Allowing negative dual variable(s) as small as -6.12734168959e-12.
Allowing negative dual variable(s) as small as -1.16461562616e-11.
Allowing negative dual variable(s) as small as -6.60170529354e-12.
Allowing negative dual variable(s) as small as -6.59680643444e-12.
Allowing negative dual variable(s) as small as -1.10062503816e-11.
Allowing negative dual variable(s) as small as -1.16812438628e-11.
Allowing negative dual variable(s) as small as -1.10529521733e-11.
Allowing negative dual variable(s) as small as -1.11136961179e-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 -1.799230708e-11.
Allowing negative dual variable(s) as small as -6.27934368998e-12.
Allowing negative dual variable(s) as small as -1.0407511658e-11.
Allowing negative dual variable(s) as small as -1.04266847977e-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 -5.91621573619e-12.
Allowing negative dual variable(s) as small as -1.29122650256e-13.
Allowing negative dual variable(s) as small as -8.83726340414e-14.
Allowing negative dual variable(s) as small as -9.08665447835e-14.
Solving took 4 GP solves and 1.9 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 -9.91019471347e-11.
Allowing negative dual variable(s) as small as -8.92994454424e-11.
Allowing negative dual variable(s) as small as -8.98728205571e-11.
Allowing negative dual variable(s) as small as -8.47866343107e-11.
Solving took 4 GP solves and 3.93 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -1.61287233569e-11.
Allowing negative dual variable(s) as small as -6.10415884505e-12.
Allowing negative dual variable(s) as small as -1.16313417231e-11.
Allowing negative dual variable(s) as small as -6.6089217432e-12.
Allowing negative dual variable(s) as small as -6.60314858347e-12.
Allowing negative dual variable(s) as small as -1.10105349317e-11.
Allowing negative dual variable(s) as small as -1.1684831271e-11.
Allowing negative dual variable(s) as small as -1.10536509416e-11.
Allowing negative dual variable(s) as small as -1.11132987578e-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 -1.79884011332e-11.
Allowing negative dual variable(s) as small as -6.27530156744e-12.
Allowing negative dual variable(s) as small as -1.04102492685e-11.
Allowing negative dual variable(s) as small as -1.04262211928e-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 -5.91637027777e-12.
Allowing negative dual variable(s) as small as -1.25811247317e-13.
Allowing negative dual variable(s) as small as -8.84660627284e-14.
Allowing negative dual variable(s) as small as -9.09344359566e-14.
Solving took 4 GP solves and 1.99 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 -9.91010181903e-11.
Allowing negative dual variable(s) as small as -8.93117632801e-11.
Allowing negative dual variable(s) as small as -8.98844210867e-11.
Allowing negative dual variable(s) as small as -8.47982873156e-11.
Solving took 4 GP solves and 4.73 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Passed

Standard Output

Standard Error
