Accession Number : AD0702194

Title :   THEORY AND DESIGN OF TURBOCOMPRESSORS,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Seleznev,K. P. ; Podobuyev,Yu. S. ; Anisimov,S. A.

Report Date : 21 NOV 1969

Pagination or Media Count : 512

Abstract : Problems dealing with the theory and design of turbocompressors based on the gas-dynamic theory of cascades are examined. The thermodynamic bases of the theory of turbomachines, the basic problems of the aerodynamics of compressible gas and elements of theory of the wing are included. Problems of the flow of gas around flat, annular, circular and three-dimensional cascade designs are expounded in sufficient detail. The theory and design of a stage of a turbocompressor are examined. (Author)

Descriptors :   (*GAS TURBINES, DESIGN), THEORY, THERMODYNAMICS, GAS FLOW, CASCADE STRUCTURES, AERODYNAMIC CHARACTERISTICS, USSR

Subject Categories : Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE