Boundary Layer Stall is a flow separation phenomenon characterized by the disruption of the laminar or turbulent boundary layer adjacent to a solid surface due to adverse pressure gradients, leading to a sudden loss of aerodynamic efficiency and marked deviation from attached flow behavior.
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Publications
549
Citations
17
Authors
19
Institutions
Publications per year
2017–2026
1
Parents
Publications
8
1–5 of 8
Authors
17
- SJ
2
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- LE
1
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- HDHenda Djéridi
Laboratoire des Écoulements Géophysiques et Industriels, France
1 publications · 24 citations
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- CS
1
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- ZM
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1–5 of 17
Institutions
19
Stanford University
Stanford, United States
2 h-index
2 publications
169 citations
Glenn Research Center
Cleveland, United States
1 h-index
1 publications
81 citations
Institut de Recherche de l’École Navale
Brest, France
1 h-index
3 publications
72 citations
Université Européenne de Bretagne
Rennes, France
1 h-index
1 publications
24 citations
American Institute of Aeronautics and Astronautics
Reston, United States
1 h-index
1 publications
25 citations
Laboratoire des Écoulements Géophysiques et Industriels
Grenoble, France
1 h-index
1 publications
24 citations
Institut Icare
Sierre, Switzerland
1 h-index
1 publications
22 citations
Institut Océanographique
Paris, France
1 h-index
1 publications
24 citations
1–8 of 19
Venues
- Journal of Basic Engineering
2 publications · 169 citations
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- International Journal of Heat and Technology
1 publications · 22 citations
1
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- University of North Texas Digital Library (University of North Texas)
Repository · 1 publications · 187 citations
1
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- Journal of Applied Mechanics
1 publications · 25 citations
1
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- Journal of Aircraft
1 publications · 68 citations
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