Accession Number : AD0272813

Title :   ROCKET EXHAUST INTO A HYPERVELOCITY STREAM. FAR FIELD ANALYSIS

Corporate Author : GENERAL DYNAMICS/POMONA CALIF

Personal Author(s) : YOSHIHARA,HIDEO

Report Date : FEB 1962

Pagination or Media Count : 1

Abstract : Far field of a rocket jet exhausting into a surrounding medium moving at hypervelocity is analyzed using the compressible turbulent NavierStokes equations simplified by the boundary layer approximations. (Author)

Descriptors :   *EXHAUST GASES, *JET MIXING FLOW, COMPRESSIBLE FLOW, GAS FLOW, HYPERSONIC CHARACTERISTICS, MATHEMATICAL ANALYSIS, ROCKET ENGINES, TRANSPORT PROPERTIES, WAKE

Distribution Statement : APPROVED FOR PUBLIC RELEASE