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Development of Wing Leading Edge Vortex Generators for a Single Engine General Aviation Airplane
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1983 by SAE International in United States
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A new method for improving spin characteristics of a General Aviation airplane has been developed and demonstrated to be very effective in providing spin damping. This concept consists of a wing leading edge vortex generating device situated to induce outboard flow attachment in the spin.
CitationCrider, D., "Development of Wing Leading Edge Vortex Generators for a Single Engine General Aviation Airplane," SAE Technical Paper 830770, 1983, https://doi.org/10.4271/830770.
- Chambers, J.R., Overview of Stall/Spin Technology, AIAA Paper 80-1580, August, 1980.
- DiCarlo, D.J., Slough, H.P., Patton, J.M., Effects of Wing Leading Edge Design on the Spin Characteristics of a General Aviation Airplane. AIAA Paper 80-1843R, March, 1981.