Development of Wing Leading Edge Vortex Generators for a Single Engine General Aviation Airplane 830770
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.
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. Download Citation
Author(s):
Dennis Crider
Affiliated:
Beech Aircraft Corp., Wichita, KS
Pages: 8
Event:
Business Aircraft Meeting and Exposition
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Business and general aviation aircraft
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