Accession Number : AD0281774
Title : RESEARCH IN HYBRID COMBUSTION.
Descriptive Note : Quarterly progress rept. for period ending 30 May 62,
Corporate Author : ROCKETDYNE CANOGA PARK CALIF
Personal Author(s) : Peck ,M. V. ; Houser,T.
Report Date : 30 JUN 1962
Pagination or Media Count : 37
Abstract : The equations derived from the simplified hybrid combustion theory based upon a diffusion flame model are applicable to turbulent gaseous flow upon proper definition of the parameters. The well-defined flame front is substantiated by movies taken at the end of the combustor. The complementary approach of examination of the solid phase heat conduction is being explored. (Author)
Descriptors : *COMBUSTION, *HYBRID ROCKET PROPELLANTS, ACRYLIC RESINS, ALUMINUM, DIFFUSION, FLAMES, GAS FLOW, GASES, HEAT TRANSFER, OXYGEN, PHOTOGRAPHIC ANALYSIS, POLYMERS, SOLIDS, SOUND MOTION PICTURE PROJECTORS, THEORY, THERMAL CONDUCTIVITY, TURBULENCE
Distribution Statement : APPROVED FOR PUBLIC RELEASE