Sweep Effects is a phenomenon in wing aerodynamics within lateral-directional flight dynamics characterized by the alteration of aerodynamic forces and moments due to the spanwise flow redistribution caused by the aft or forward inclination of the wing leading edge relative to the freestream direction.
129
Publications
4.6K
Citations
279
Authors
127
Institutions
Publications per year
2017–2026
18
Variants
Wing Sweep Effects
Publications
129
1–5 of 129
Authors
279
- GP
4
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- IG
3
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- JM
3
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- NW
3
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- WF
3
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1–5 of 279
Institutions
127
Langley Research Center
Hampton, United States
6 h-index
6 publications
269 citations
Utah State University
Logan, United States
5 h-index
12 publications
203 citations
University of Cambridge
Cambridge, United Kingdom
5 h-index
9 publications
177 citations
University of Bath
Bath, United Kingdom
3 h-index
6 publications
161 citations
Ames Research Center
Mountain View, United States
3 h-index
4 publications
103 citations
Delft University of Technology
Delft, The Netherlands
3 h-index
7 publications
135 citations
Shell (Netherlands)
The Hague, The Netherlands
3 h-index
4 publications
131 citations
Rolls-Royce (United Kingdom)
London, United Kingdom
3 h-index
3 publications
55 citations
1–8 of 127
Venues
- Journal of Aircraft
11 publications · 312 citations
10
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- AIAA Journal
8 publications · 459 citations
8
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- Journal of Turbomachinery
7 publications · 294 citations
7
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- University of North Texas Digital Library (University of North Texas)
Repository · 6 publications · 199 citations
6
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- NASA Technical Reports Server (NASA)
Repository · 4 publications · 88 citations
4
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