Accession Number : AD0727175

Title :   Aircraft Engines (Selected Articles)

Corporate Author : AIR FORCE SYSTEMS COMMAND WRIGHT-PATTERSON AFB OH FOREIGN TECHNOLOGY DIVISION

Personal Author(s) : Bordovitsyn, Yu A ; Kalmykov, I I ; Strunkin, V A ; Dyatlov, I N ; Sharapov, A V

PDF Url : AD0727175

Report Date : 07 May 1971

Pagination or Media Count : 88

Abstract : ;Contents: The effect of the form of an active gas jet on the characteristics of a gas ejector with short mixing chamber; Calculation of the maximum degree of compression of an ejector; The rational method of selecting parameters and calculating single-stage gas turbines; A generalization of the results of measurements of the fineness of fuel atomization of mechanical and air-mechanical injectors of the pressure-jet type; Calculation of temperature field in a cooled turbine blade with longitudinal cooling channels; Turbulence in the zone of interplay of jetstreams with the flow.

Descriptors :   *AIRCRAFT ENGINES, *COMBUSTION, ATOMIZATION, COMBUSTION CHAMBERS, EJECTION, FLOW FIELDS, GAS TURBINE BLADES, GAS TURBINES, MATHEMATICAL MODELS, NOZZLES, REPORTS, USSR

Subject Categories : Combustion and Ignition
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE