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Volumn 21, Issue 2, 2007, Pages 1-7

Experimental investigation on flow structures over nonslender delta wings at low Reynolds numbers

Author keywords

Flow visualization; Low Reynolds number flow; Nonslender delta wing; Vortex structure

Indexed keywords

AERODYNAMICS; FLOW STRUCTURE; FLOW VISUALIZATION; REYNOLDS NUMBER; VORTEX FLOW;

EID: 34547326056     PISSN: 16729897     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (12)

References (13)
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  • 2
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    • Three-dimensional flow structure on delta wings at high angle-of-attack: experimental concepts and issues
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  • 3
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    • Survey of research on unsteady aerodynamic loading of delta wings
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  • 5
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  • 7
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    • Effects of leading-edge shape and vortex burst on the flowfield of a 70° sweep delta wing
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    • KEGELMAN J, ROOS F. Effects of leading-edge shape and vortex burst on the flowfield of a 70° sweep delta wing[R]. AIAA 89-0086, 1989.
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  • 8
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    • Flow developments above 50° sweep delta wings with different leading-edge profiles
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  • 9
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    • Higher-order compact difference scheme applied to the simulation of a low sweep delta wing flow
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    • GORDNIER R E, VISBAL M R. Higher-order compact difference scheme applied to the simulation of a low sweep delta wing flow[R]. AIAA, 2003-620, 2003.
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  • 10
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    • An investigation of vortex flows over low sweep delta wings
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  • 11
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    • Leading-edge vortex structure of non-slender delta wings at low Reynolds number
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  • 12
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.