830770: Development of Wing Leading Edge Vortex Generators for a Single Engine General Aviation Airplane - Technical Paper

Event: Business Aircraft Meeting and Exposition

Authors

Beech Aircraft Corp., Wichita, KS

Abstract

Content: 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.

Meta Tags

Topics: Business and general aviation aircraft

Affiliated or Co-Author: Beech Aircraft Corp., Wichita, KS

Details

DOI: https://doi.org/10.4271/830770

Pages: 8

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.

Additional Details

Publisher: SAE International

Published: Feb 1, 1983

Product Code: 830770

Content Type: Technical Paper

Language: English