Investigation of distributions of pressure, recovery factor, and heat-transfer coefficient on 20° cones incorporating annular cavities was carried out in helium at free-stream Mach numbers of 11; effects of Reynolds number, cavity length-depth ratio, and reattachment region geometry were studied with emphasis on laminar, open cavity flow regime; results showed that pressure was virtually constant within cavity and downstream and very close to laminar attached-flow value.
Study of laminar hypersonic cavity flows
AIAA J
AIAA Journal ; 2 , n 9
1964
7 pages
Aufsatz (Zeitschrift)
Englisch
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A study of laminar hypersonic cavity flows
AIAA | 1964
|A study of laminar hypersonic cavity flows
AIAA | 1964
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AIAA | 1974
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