Accession Number : AD0769747

Title :   Investigations into the Variation of the Internal Ballistics of a Solid Fuel Ramjet Through Combustor Design.

Descriptive Note : Master's thesis,

Corporate Author : NAVAL POSTGRADUATE SCHOOL MONTEREY CALIF

Personal Author(s) : Jones,Charles Ernest , III

Report Date : SEP 1973

Pagination or Media Count : 77

Abstract : An experimental investigation of the internal ballistics of solid fuel ramjets was conducted in order to more adequately define the pertinent variables in combustor design. The experimental investigation included the effects of wall mass addition on the recirculation zone of a rearward facing step combustor design, various methods of combustor flame stabilization, and the effects of inlet turbulence on the internal ballistics of the combustor. Flow conditions within the recirculation zone were unaffected by varying rates of wall mass addition. Swirl devices and centerbodies were found to be inadequate substitutes for the rearward facing step inlet. The solid fuel ramjet combustor was found to be highly susceptible to inlet turbulence. (Modified author abstract)

Descriptors :   (*Combustion chambers, Interior ballistics), (*Ramjet engines, *Solid jet engine fuels), Experimental design, Duct inlets, Flow visualization, Jet flames, Stability, Recirculation, Turbulence, Theses

Subject Categories : Combustion and Ignition
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE