Slat Aerodynamics
Slat Aerodynamics is a subfield of wing aerodynamics that investigates the flow phenomena and performance enhancements generated by the deployment of leading-edge slats on lifting surfaces, distinguished by its focus on high-lift configuration behavior at low speeds.
68
Publications
2.4K
Citations
175
Authors
49
Institutions
Publications per year
2017–2026
10
68
Noise Radiation from a Leading-Edge Slat
David P. Lockard, Meelan M. Choudhari · 2009 · 90 citations · Full text
Engineering, Aerospace Engineering, Mechanical Engineering +17
Flow over an aerofoil without and with a leading-edge slat at a transitional Reynolds number
Mustafa Serdar Genç, Ünver Kaẏnak, Gary D. Lock · Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering · 2009 · 89 citations
Engineering, Aerospace Engineering, Computational Engineering +17
1–5 of 68
175
7
h-index
4
h-index
4
h-index
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
3 publications · 76 citations
3
h-index
3
h-index
1–5 of 175
49

Langley Research Center
Hampton, United States
14 h-index
35 publications
1.3K citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
4 h-index
13 publications
302 citations
Science and Technology Corporation (United States)
Hampton, United States
4 h-index
7 publications
155 citations
Japan Aerospace Exploration Agency
Tokyo, Japan
4 h-index
17 publications
440 citations
University of California, Davis
Davis, United States
3 h-index
4 publications
56 citations

University of Notre Dame
Notre Dame, United States
3 h-index
9 publications
198 citations

Ames Research Center
Mountain View, United States
3 h-index
8 publications
436 citations
Georgia Institute of Technology
Atlanta, United States
3 h-index
5 publications
70 citations
1–8 of 49
12 publications · 301 citations
12
h-index
4 publications · 438 citations
4
h-index
Repository · 3 publications · 64 citations
3
h-index
2 publications · 79 citations
2
h-index
JSV · 2 publications · 76 citations
2
h-index
1–5