Accession Number : ADD000321

Title :   Compact High Thrust Augmentation Ejector System.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C

Personal Author(s) : Quinn,Brian P

Report Date : 10 Sep 1974

Pagination or Media Count : 9

Abstract : In the invention an ejector system is provided which makes use of hypermixing nozzles, together with root nozzles which substantially reduce the losses associated with the inlet region, the primary air nozzle, the mixing region and the diffuser.

Descriptors :   *Thrust augmentation, *Patents, Thrust augmentor nozzles, Diffusers, Vertical takeoff aircraft, Short takeoff aircraft, Ejectors

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE