Fowler Flap Design
Fowler Flap Design is a high-lift device configuration in aerospace engineering that belongs to the class of trailing-edge flap systems and is distinguished by its mechanism of increasing wing area and camber through simultaneous rearward translation and downward deflection of the flap surface.
10
Publications
240
Citations
16
Authors
4
Institutions
Publications per year
2017–2026
1
Parents
10
1–5 of 10
16
4
h-index
2
h-index
1
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1
h-index
1 publications · 18 citations
1
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1–5 of 16
4
Wichita State University
Wichita, United States
4 h-index
5 publications
125 citations

Boeing (United States)
Chicago, United States
1 h-index
1 publications
26 citations
Georgia Institute of Technology
Atlanta, United States
1 h-index
2 publications
52 citations

Beihang University
Beijing, China
1 h-index
4 publications
116 citations
University of Kansas
Lawrence, United States
1 publications
11 citations
Flexsys (United States)
Ann Arbor, United States
1 publications
14 citations
Jacobs (United States)
Dallas, United States
1 publications
14 citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
1 publications
14 citations
1–8 of 4
3 publications · 45 citations
3
h-index
Repository · 2 publications · 38 citations
2
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Repository · 2 publications · 67 citations
2
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1 publications · 35 citations
1
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1 publications · 26 citations
1
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1–5