Control Surface Buzz
Control Surface Buzz is a dynamic aeroelastic instability, typically manifesting as a self-excited, single-degree-of-freedom limit-cycle oscillation of an aircraft trailing-edge control surface about its hinge, driven by unsteady interactions between transonic shock waves and the boundary layer over the surface.
6
Publications
116
Citations
22
Authors
8
Institutions
Publications per year
2017–2026
1
6
Stall Control with Local Surface Buzzing on a NACA 0012 Airfoil
Y. W. Park, Soogab Lee, Dong‐Ho Lee et al. · AIAA Journal · 2001 · 20 citations
1–5 of 6
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8
Northrop Grumman (United States)
Falls Church, United States
1 h-index
1 publications
30 citations
Lockheed Martin (United States)
Bethesda, United States
1 h-index
1 publications
30 citations

Boeing (United States)
Chicago, United States
1 h-index
2 publications
20 citations

Harbin Institute of Technology
Harbin, China
1 h-index
5 publications
115 citations
Heilongjiang Institute of Technology
Harbin, China
1 h-index
5 publications
115 citations
Seoul National University
Seoul, South Korea
1 h-index
4 publications
80 citations

Northwestern Polytechnical University
Xi'an, China
1 h-index
3 publications
54 citations

Langley Research Center
Hampton, United States
1 h-index
1 publications
30 citations
1–8 of 8
1 publications · 18 citations
1
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1 publications · 30 citations
1
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1 publications · 20 citations
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AST · 1 publications · 23 citations
1
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Conference · 1 publications · 15 citations
1
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1–5