Accession Number : ADD005006

Title :   Finned Surface Cooled Nozzle.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C

Personal Author(s) : Sutton,Joel F ; Mattson,Allen R ; Anders,Larry E

Report Date : 28 Mar 1978

Pagination or Media Count : 15

Abstract : This patent describes an air-cooled, variable-throat, convergent-divergent nozzle for a turbojet engine.

Descriptors :   *Patents, *Convergent divergent nozzles, *Variable area nozzles, Turbojet engines, Air cooled, Air intakes, Jet engine exhaust

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE