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Title of Article

INVESTIGATION OF THRUST VECTORING METHODS IN EJECTOR AND TURNING NOZZLES


Issue
4
Date
2011

Article type
scientific article
UDC
533.694.6
Pages
692-693
Keywords
 


Authors
Vorobev S.V.
Tsentralnyy institut aviatsionnogo motorostroeniya im. P.I. Baranova, Moskva

Klestov Yu.M.
Tsentralnyy institut aviatsionnogo motorostroeniya im. P.I. Baranova, Moskva

Myshenkov E.V.
Tsentralnyy institut aviatsionnogo motorostroeniya im. P.I. Baranova, Moskva

Myshenkova E.V.
Moskovskiy energeticheskiy institut (tekhnicheskiy universitet)


Abstract
The report presents results of experimental and theoretical investigations of nozzles with thrust vectoring conducted in Central Institute of Aviation Motors. The nozzles includes nozzles with turning supersonic, flat and 3D nozzles with asymmetric ejection of ambient flow, nozzles with injections and interceptors, and nozzles with critical surface shifting.

File (in Russian)