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Development of Wing Leading Edge Vortex Generators for a Single Engine General Aviation Airplane Beech Aircraft Corporation, Wichita, KS

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Crider, Dennis, author.
Conference Name:
Business Aircraft Meeting and Exposition (1983-04-12 : Wichita, Kansas, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1983
Summary:
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
Notes:
Vendor supplied data
Publisher Number:
830770
Access Restriction:
Restricted for use by site license

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