Accession Number : AD0770061
Title : Supersonic Combustion and Burning in Ramjet Combustors.
Descriptive Note : Final rept. 1 Apr 72-31 Mar 73,
Corporate Author : OHIO STATE UNIV RESEARCH FOUNDATION COLUMBUS
Personal Author(s) : Edse,Rudolph ; Rice,E. E. ; Kitzmiller,C. T.
Report Date : JUL 1973
Pagination or Media Count : 199
Abstract : The report contains research results obtained from experimental and theoretical studies of subsonic and supersonic burning in ramjet combustors during the period 1 April 1972 to 31 March 1973. Hydrogen-oxygen mixtures sensitized by chlorine have been ignited photochemically at flow speeds from 350-550 m/s and photochemical ignition limits have been measured at pressures between 100 and 400 mmHg. The formation of weak detonation has been observed. Calculated ignition delay times have been found to agree satisfactorily with experimental values. Tables and graphs have been prepared for quick predictions of the changes resulting from heat addition to an existing sub- or supersonic flow, such as those in ramjet combustors. (Modified author abstract)
Descriptors : (*Combustion chambers, *Supersonic combustion), (*Supersonic combustion ramjet engines, Combustion chambers), Photochemical reactions, Supersonic flow, Ignition lag, Flame arresters, Reaction kinetics, Exhaust nozzles
Subject Categories : Combustion and Ignition
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE