Accession Number : AD0615985

Title :   PULSATING COMBUSTION OF GAS BEHIND A SHOCK WAVE IN SUPERSONIC FLOW,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Soloukhin,R. I.

Report Date : 13 MAY 1965

Pagination or Media Count : 8

Abstract : In the experiments described a shock tube was used to obtain a stream of mixture, in which the temperature behind the front of direct densification jump at the surface of the decelerating body is sufficient for adiabatic spontaneous combustion of the gas. The condition of periodic ignition of the gas behind the disconnected shock wave was investigated.

Descriptors :   (*COMBUSTION, GASES), IGNITION, SHOCK WAVES, SUPERSONIC FLOW, DETONATIONS, USSR

Distribution Statement : APPROVED FOR PUBLIC RELEASE