Wing Twist Effects
Wing Twist Effects is a static aeroelastic phenomenon characterized by the alteration of an aircraft wing's aerodynamic performance due to elastic torsional deformation induced by aerodynamic loads, distinguishing it from other aeroelastic effects by its primary influence on lift distribution and stall characteristics through changes in local angle of attack.
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Tuyen Quang Le, Tien Van Truong, Soo Hyung Park et al. · Journal of The Royal Society Interface · 2013 · 74 citations · Full text
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Utah State University
Logan, United States
3 h-index
6 publications
374 citations

Konkuk University
Seoul, South Korea
3 h-index
10 publications
527 citations

Langley Research Center
Hampton, United States
3 h-index
6 publications
298 citations
Cranfield University
Cranfield, United Kingdom
2 h-index
4 publications
82 citations

University of Exeter
Exeter, United Kingdom
2 h-index
2 publications
210 citations
Korea Institute of Ocean Science and Technology
Busan, South Korea
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3 publications
193 citations
Loughborough University
Loughborough, United Kingdom
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1 publications
15 citations
Sungkyunkwan University
Seoul, South Korea
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1 publications
74 citations
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7 publications · 270 citations
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AST · 2 publications · 63 citations
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2 publications · 210 citations
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Repository · 2 publications · 26 citations
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