Accession Number : AD0681597

Title :   TRANSITION OF A COMBUSTION MIXTURE FROM SUPERSONIC FLOW TO THE CHAPMAN-JOUGET REGIME,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Gilinskii,S. M. ; Zapryanov,Z. D.

Report Date : 30 JUL 1968

Pagination or Media Count : 15

Abstract : The investigation of supersonic flow about bodies by a combustion mixture of gases is of importance in studying combustion efficiency of fuel in ramjet engines. In the present study, a numerical method is presented for solving the problem of supersonic flow about a cylinder and a plate with a cylindrical bluntness. A study was also made of a possible transition to the Chapman-Jouget regime.

Descriptors :   (*SUPERSONIC COMBUSTION, FLOW FIELDS), (*DETONATION WAVES, STABILIZATION), SUPERSONIC COMBUSTION RAMJET ENGINES, SUPERSONIC FLOW, CYLINDRICAL BODIES, BLUNT BODIES, FLAT PLATE MODELS, NUMERICAL METHODS AND PROCEDURES, TURBULENCE, PRESSURE, USSR

Subject Categories : Combustion and Ignition

Distribution Statement : APPROVED FOR PUBLIC RELEASE