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