Accession Number:
AD0272813
Title:
ROCKET EXHAUST INTO A HYPERVELOCITY STREAM. FAR FIELD ANALYSIS
Descriptive Note:
Corporate Author:
GENERAL DYNAMICS/POMONA CALIF
Personal Author(s):
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