Accession Number:

AD0272813

Title:

ROCKET EXHAUST INTO A HYPERVELOCITY STREAM. FAR FIELD ANALYSIS

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/POMONA CALIF

Personal Author(s):

• YOSHIHARA,HIDEO

Report Date:

1962-02-01

Pagination or Media Count:

1.0

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

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE