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Volumn 25, Issue 7, 2008, Pages 2550-2553
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Experimental investigations on leading-edge vortex structures for flow over non-slender delta wings
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Author keywords
[No Author keywords available]
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Indexed keywords
ANGLE OF ATTACK;
REYNOLDS NUMBER;
VORTEX FLOW;
ANGLE-OF-ATTACK;
DELTA WINGS;
DYE-INJECTION;
EXPERIMENTAL INVESTIGATIONS;
HYDROGEN BUBBLES;
LEADING-EDGE VORTICES;
REYNOLD NUMBER;
SWEEP ANGLE;
VORTEX CORES;
VORTEX STRUCTURES;
DELTA WING AIRCRAFT;
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EID: 46749142551
PISSN: 0256307X
EISSN: 17413540
Source Type: Journal
DOI: 10.1088/0256-307X/25/7/060 Document Type: Article |
Times cited : (27)
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References (12)
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