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Development of Wing Leading Edge Vortex Generators for a Single Engine General Aviation Airplane
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English
Abstract
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.
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Citation
Crider, 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.Also In
References
- Chambers, J.R. Overview of Stall/Spin Technology AIAA Paper 80-1580 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 1981