Accession Number : AD0684639

Title :   SUPERSONIC FLOW AROUND OF A SPHERE BY A COMBUSTIBLE MIXTURE OF GASES WITH CONSIDERATION OF IGNITION DELAY TIME,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Gilinskii,S. M. ; Chernyi,G. G.

Report Date : 23 AUG 1968

Pagination or Media Count : 29

Abstract : A numerical resolution is given of the problem of flow around a sphere by a fuel mixture with the simplest model of the structure of the burn zone in which the whole flow after the forward shock consists of two regions of adiabatic flow - the induction region and the region of equilibrium flow of combustion products, divided by the burn front, in which the mixture burns instantly. A solution is given only for the subsonic and transonic regions of flow. (Author)

Descriptors :   (*SUPERSONIC COMBUSTION, SUPERSONIC FLOW), BURNING RATE, SPHERES, IGNITION LAG, NUMERICAL ANALYSIS, FUELS, MIXTURES, ADIABATIC GAS FLOW, USSR

Subject Categories : Combustion and Ignition

Distribution Statement : APPROVED FOR PUBLIC RELEASE