Variable Angle Jet Flap System.
Abstract
The patent application relates to a variable angle jet flap for control of aerodynamic flow across an airborne airfoil.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 14, 1972
- Accession Number
- AD0164463
Entities
People
- J. W. Headley
Organizations
- United States Department of the Air Force