Tail Aeroelasticity
Tail Aeroelasticity is a specialized aeroelastic phenomenon characterized by the dynamic interaction between aerodynamic forces, structural elasticity, and inertial effects specific to the tail section of an aircraft, distinguishing it from aeroelastic behaviors in other airframe components.
6
Publications
250
Citations
21
Authors
11
Institutions
Publications per year
2017–2026
1
Parents
6
Active vibration-suppression systems applied to twin-tail buffeting
Mark A. Hopkins, Douglas A. Henderson, Robert W. Moses et al. · Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE · 1998 · 36 citations
Engineering, Aerospace Engineering, Mechanical Engineering +17
1–5 of 6
21
United States Air Force Research Laboratory, United States
2 publications · 72 citations
2
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1
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1
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1
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1
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1–5 of 21
11

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
2 h-index
3 publications
108 citations
Lockheed Martin (United States)
Bethesda, United States
1 h-index
2 publications
20 citations
China Jiliang University
Hangzhou, China
1 h-index
2 publications
40 citations
National Research Council Canada
Ottawa, Canada
1 h-index
1 publications
36 citations

Wright-Patterson Air Force Base
Wright-Patterson AFB, United States
1 h-index
1 publications
36 citations
University of Cambridge
Cambridge, United Kingdom
1 h-index
2 publications
274 citations
Georgia Institute of Technology
Atlanta, United States
1 h-index
3 publications
108 citations

Nanjing University of Aeronautics and Astronautics
Nanjing, China
1 h-index
4 publications
80 citations
1–8 of 11
1 publications · 36 citations
1
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1 publications · 36 citations
1
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1 publications · 137 citations
1
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1 publications · 20 citations
1
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1 publications · 11 citations
1
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1–5