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Volumn 39, Issue 4, 2001, Pages 654-659
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Temperature- and pressure-sensitive paint measurements in short-duration hypersonic flow
d
CUBRC
(United States)
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Author keywords
[No Author keywords available]
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Indexed keywords
BOUNDARY LAYERS;
HEAT TRANSFER;
HYPERSONIC FLOW;
LAMINAR FLOW;
PAINT;
SHOCK WAVES;
THIN FILMS;
TRANSITION FLOW;
TURBULENT FLOW;
WIND TUNNELS;
HYPERSONIC SHOCK TUNNELS;
SENSITIVE PAINT MEASUREMENTS;
HYPERSONIC AERODYNAMICS;
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EID: 0035311410
PISSN: 00011452
EISSN: None
Source Type: Journal
DOI: 10.2514/2.1358 Document Type: Article |
Times cited : (56)
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References (15)
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