SIMILTUDE LAWS FOR A FLOW OF GAS IN A THIN HYPERSONIC NOZZLE,

reportActive / Technical Report | Accession Number: AD0625787 | Need Help?

Abstract:

A similitude law for flow of gas in a hypersonic nozzle taking into account the interactions of the boundary layer with a potential nucleus similar to a previously established similitude law for external flow past thin bodies is obtained. Author

Author(s):
Zhilin, Yu. L.
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Supplementary Note:
Unedited rough draft trans. of Inzhenernyi Zhurnal (USSR) v3 n4 p628-31 1963. Supersedes trans. dated 2 Jul 65.
Annotation:
Translation of Russian research: Similitude laws for a flow of gas in a thin hypersonic nozzle.
Pagination:
0011

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-TT-65-690, TT-66-60135
Monitor Series:
66-60135
 Subject Terms
Modernization Areas:
Hypersonics
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*NOZZLE GAS FLOW, HYPERSONIC FLOW, PERTURBATIONS, SIMULATION, USSR, BOUNDARY LAYER
Field(s)/Group(s):
Fluid Mechanics
Keyword(s):
ANALOGIES
Report Date:
1965 Oct 26