Trailing-edge Flap Design
Trailing-Edge Flap Design is a high-lift system design methodology that specifically involves the configuration and optimization of movable aerodynamic surfaces on the trailing edge of an aircraft wing to enhance lift during low-speed flight phases.
125
Publications
4K
Citations
328
Authors
107
Institutions
Publications per year
2017–2026
25
Parents
125
1–5 of 125
328
12
h-index
5
h-index
5
h-index
5
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5
h-index
1–5 of 328
107
University of Maryland, College Park
College Park, United States
12 h-index
30 publications
905 citations

Ames Research Center
Mountain View, United States
8 h-index
11 publications
495 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
7 h-index
19 publications
764 citations

Indian Institute of Science Bangalore
Bengaluru, India
5 h-index
12 publications
313 citations
University of Washington
Seattle, United States
4 h-index
6 publications
267 citations

Boeing (United States)
Chicago, United States
4 h-index
9 publications
604 citations
Massachusetts Institute of Technology
Cambridge, United States
4 h-index
7 publications
395 citations

University of Bristol
Bristol, United Kingdom
4 h-index
18 publications
1K citations
1–8 of 107
11 publications · 334 citations
11
h-index
10 publications · 319 citations
10
h-index
9 publications · 194 citations
9
h-index
SMS · 6 publications · 412 citations
6
h-index
JIMSS · 5 publications · 430 citations
5
h-index
1–5