Accession Number : AD0653541

Title :   FLIGHT REGIMES OF A VEHICLE WITH A RAMJET ENGINE WHICH PROVIDE FOR CONSTANT CONDITIONS OF FLAME STABILIZATION,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Gruzdev,V. N. ; Talantov,A. V.

Report Date : 28 FEB 1967

Pagination or Media Count : 17

Abstract : An attempt is made to find the flight regimes of a vehicle with a ramjet engine which permits operation of the combustion chamber without flameout. The conditions of flame stabilization in a straight-through combustion chamber with the aid of poorly streamlined bodies (mechanical stabilizers) to a significant extent depend on the physical parameters of the mixture that enters the chamber, i.e., pressure and temperature. The latter, in turn, are functions of the flight regime of the vehicle, i.e., the velocity and altitude of flight (M and H). Thus, the conditions of flame stabilization, in the final result, are determined by the flight regime of the vehicle.

Descriptors :   (*RAMJET ENGINES, PERFORMANCE(ENGINEERING)), (*COMBUSTION, STABILIZATION), FLAMES, COMBUSTION CHAMBERS, OPTIMIZATION, FLIGHT, VELOCITY, ALTITUDE, SHOCK WAVES, FLAMEOUT, USSR

Subject Categories : Combustion and Ignition
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE