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.
Development of Wing Leading Edge Vortex Generators for a Single Engine General Aviation Airplane
Sae Technical Papers
Business Aircraft Meeting and Exposition ; 1983
1983-02-01
Aufsatz (Konferenz)
Englisch