Accession Number : AD0164463

Title :   Variable Angle Jet Flap System.

Descriptive Note : Patent Application,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C

Personal Author(s) : Headley,J. W.

Report Date : 14 NOV 1972

Pagination or Media Count : 10

Abstract : The patent application relates to a variable angle jet flap for control of aerodynamic flow across an airborne airfoil.

Descriptors :   *Jet flaps, Patents, Wings, Trailing edge, Boundary layer control

Subject Categories : Aerodynamics
      Aircraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE