Wing Stall is a fluid-dynamic phenomenon characterized by the abrupt reduction in lift generation due to flow separation over a wing when the critical angle of attack is exceeded.
117
Publications
4.2K
Citations
249
Authors
108
Institutions
Publications per year
2017–2026
15
Parents
Publications
117
Flow over a Wing with Leading-Edge Undulations
Alex Skillen, Alistair Revell, Alfredo Pinelli et al. · AIAA Journal · 2014 · 146 citations · Full text
Investigation of Three-Dimensional Dynamic Stall Using Computational Fluid Dynamics
A. Spentzos, George N. Barakos, K. J. Badcock et al. · AIAA Journal · 2005 · 141 citations
1–5 of 117
Authors
249
- RM
12
h-index
- SH
10
h-index
- DB
8
h-index
- FJ
7
h-index
- JR
6
h-index
1–5 of 249
Institutions
108
Langley Research Center
Hampton, United States
17 h-index
65 publications
1.4K citations
Naval Air Systems Command
NAS Pax River, United States
11 h-index
19 publications
365 citations
United States Air Force Academy
Colorado Springs, United States
6 h-index
8 publications
203 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
4 h-index
5 publications
246 citations
Lockheed Martin (United States)
Bethesda, United States
4 h-index
4 publications
113 citations
Wright-Patterson Air Force Base
Wright-Patterson AFB, United States
3 h-index
6 publications
243 citations
Hartford Financial Services (United States)
Hartford, United States
3 h-index
5 publications
167 citations
San Diego State University
San Diego, United States
3 h-index
6 publications
224 citations
1–8 of 108
Venues
- Journal of Aircraft
27 publications · 858 citations
18
h-index
- AIAA Journal
12 publications · 1.1K citations
12
h-index
- 41st Aerospace Sciences Meeting and Exhibit
14 publications · 275 citations
12
h-index
- SAE technical papers on CD-ROM/SAE technical paper series
4 publications · 67 citations
4
h-index
- Physics of Fluids
3 publications · 99 citations
3
h-index
1–5