Shock Boundary-layer Interaction
Shock Boundary-Layer Interaction is a fluid dynamic phenomenon in compressible flow where a shock wave interacts with a nearby boundary layer, leading to adverse pressure gradients, flow separation, and altered aerodynamic performance.
616
Publications
24.9K
Citations
1.3K
Authors
352
Institutions
Publications per year
2017–2026
172
Variants
Sbli
Parents
616
Large-Eddy Simulation of the Shock/Turbulence Interaction
F. Ducros, V. Ferrand, Franck Nicoud et al. · Journal of Computational Physics · 1999 · 779 citations
1–5 of 616
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North Carolina State University, United States
10 publications · 476 citations
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Langley Research Center
Hampton, United States
19 h-index
32 publications
1.5K citations

Ames Research Center
Mountain View, United States
17 h-index
46 publications
7K citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
17 h-index
48 publications
2.1K citations
North Carolina State University
Raleigh, United States
17 h-index
40 publications
1.6K citations
University of Cambridge
Cambridge, United Kingdom
15 h-index
36 publications
1.9K citations

Glenn Research Center
Cleveland, United States
15 h-index
40 publications
1.2K citations
Princeton University
Princeton, United States
13 h-index
39 publications
2.5K citations
University of Maryland, College Park
College Park, United States
12 h-index
23 publications
1K citations
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99 publications · 7K citations
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31 publications · 1.2K citations
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22 publications · 2.8K citations
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24 publications · 940 citations
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20 publications · 905 citations
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