Accession Number : AD0756102

Title :   Conditions for the Existence of a Normal Shock Wave in the Elements of Axial Supersonic Compressor,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Vasilev,Yu. N. ; Freyman,G. A.

Report Date : 05 FEB 1973

Pagination or Media Count : 27

Abstract : Due to the rise of velocities in the running section of a compressor, of ever increasing interest is the problem dealing with stagnation of supersonic swirling flows in shock waves. In this work, conditions are found for the existence of a normal shock wave in the interblade channels of a rotor and the stator of the axial supersonic stage with a finite number of blades, and equations which permit one to calculate flows satisfying these conditions are given. (Author)

Descriptors :   (*AXIAL FLOW COMPRESSORS, SHOCK WAVES), SUPERSONIC FLOW, STAGNATION POINT, OSCILLATION, STABILITY, COMPRESSOR ROTORS, COMPRESSOR STATORS, USSR

Subject Categories : Hydraulic and Pneumatic Equipment
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE