Computational fluid dynamics including dynamic stability using USM3D Navier-Stokes.
Finite element analysis completed. CFR-title 14, subpart 23 using AGATE design allowables.
Specifications
Design V-Speeds | |
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VS0 Stall - w/Flaps @1400 lbs | 50 mph TAS @2000 ft |
VS1 Stall - Clean @1400 lbs | 55 mph TAS @2000 ft |
VH Max Level Flight | 230 mph TAS @10,000 ft (stock IO-375) |
VH Max Level Flight | 250 mph TAS @10,000 ft (Ly-con modified IO-360) |
Design Loading and Flight Envelope | |
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Limit Load @ Gross Weight | +6/-3 Gs (+1.5 safety factor) |
VFE Max Full Flaps | 100 KIAS |
Weights and Dimensions | |
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Empty Weight | 1095 lbs |
Gross Weight | 1840 lbs |
Wing Span | 28.7 ft |
Wing Area | 114.85 sq ft |
Wing Loading @ Gross Weight | 16.02 lbs per sq ft |
Wing Aspect Ratio | 7.17 |
Washout | .8053° |
Aircraft Length | 21.46 ft |
Height | 8.15 ft |
Cabin Width | 46 in |
Fuel | 46 gal |
Baggage | 107 lbs |