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