SUPERSONIC GAS FLOWS IN PERFORATED BOUNDARIES,

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Abstract:

The book presents the results of the numerous research works performed by the authors in the period 1949-51 on the effect of perforated boundaries on supersonic-flow structures. In particular, it presents the results of theoretical and experimental investigations of new general properties of supersonic-gas flows in perforated boundaries. Methods of regulating the M number in rigid nozzles, straightening of supersonic flows, and increasing of permissible test model sizes in supersonic wind tunnels are described. Author

Author(s):
Grodzovskii, G. L. ; Nikolskii, A. A. ; Svishchev, G. P. ; Taganov, G. I.
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Supplementary Note:
Unedited rough draft trans. of mono. Sverkhzvukovye Techeniya Gaza v Perforirovannykh Granitsakh, Moscow, 1967 p1-144.
Annotation:
Supersonic gas flows in perforated boundaries--Translation.
Pagination:
0149

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-HT-23-1519-67
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
(*SUPERSONIC FLOW, POROUS MATERIALS), MACH NUMBER, NOZZLE GAS FLOW, WIND TUNNEL MODELS, SUPERSONIC CHARACTERISTICS, BOUNDARY LAYER, ORIFICES, INTERACTIONS, USSR
Field(s)/Group(s):
Aerodynamics, Fluid Mechanics
Keyword(s):
TRANSLATIONS
Report Date:
1968 Mar 04