Trailing-edge Design
Trailing-Edge Design is a method in airfoil theory that specifies the geometric and aerodynamic configuration of the aftmost region of an airfoil to optimize flow attachment, minimize drag, and control vortex shedding at the boundary layer exit.
115
Publications
4K
Citations
338
Authors
126
Institutions
Publications per year
2017–2026
41
Parents
115
Jonathan D. Bartley-Cho, Donny P. Wang, Christopher Martin et al. · Journal of Intelligent Material Systems and Structures · 2004 · 136 citations
Engineering, Aerospace Engineering, Mechanical Engineering +16
1–5 of 115
338
5
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Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
5 publications · 313 citations
5
h-index
5
h-index
4
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4
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1–5 of 338
126

Delft University of Technology
Delft, The Netherlands
7 h-index
26 publications
802 citations
University of Michigan
Ann Arbor, United States
6 h-index
12 publications
526 citations
Italian Aerospace Research Centre
Capua, Italy
4 h-index
8 publications
347 citations

Northwestern Polytechnical University
Xi'an, China
4 h-index
8 publications
337 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
4 h-index
10 publications
984 citations

Harbin Institute of Technology
Harbin, China
4 h-index
19 publications
347 citations
Technical University of Denmark
Kongens Lyngby, Denmark
3 h-index
8 publications
167 citations

Langley Research Center
Hampton, United States
3 h-index
3 publications
111 citations
1–8 of 126
AST · 7 publications · 261 citations
7
h-index
6 publications · 130 citations
6
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JSV · 5 publications · 185 citations
5
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3 publications · 133 citations
4
h-index
4 publications · 291 citations
4
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1–5