Nonlinear Panel Flutter is a nonlinear aeroelastic phenomenon characterized by the dynamic instability of thin elastic panels in supersonic or hypersonic airflow, where large deformations, material nonlinearities, or geometric imperfections fundamentally alter the flutter onset and post-flutter behavior compared to classical linear panel flutter.
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91
A Finite-Element Approach for Nonlinear Panel Flutter
AIAA Journal · 1977 · 107 citations
Engineering, Computational Engineering, Mechanical Engineering +14
1–5 of 91
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149
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17
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6
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6
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6
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- MRMiguel R. Visbal
United States Air Force Research Laboratory, United States
5 publications · 260 citations
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79
Old Dominion University
Norfolk, United States
18 h-index
51 publications
3.6K citations
Northwestern Polytechnical University
Xi'an, China
8 h-index
20 publications
591 citations
Universidade do Porto
Porto, Portugal
6 h-index
6 publications
161 citations
Langley Research Center
Hampton, United States
6 h-index
7 publications
388 citations
Universidade de São Paulo
São Paulo, Brazil
6 h-index
11 publications
291 citations
Seoul National University
Seoul, South Korea
5 h-index
9 publications
410 citations
Dominion University College
Accra, Ghana
4 h-index
8 publications
146 citations
United States Air Force Research Laboratory
Wright-Patterson AFB, United States
4 h-index
6 publications
430 citations
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- AIAA Journal
32 publications · 1.8K citations
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- Composite Structures
11 publications · 377 citations
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- Journal of Aircraft
6 publications · 136 citations
6
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- International Journal of Non-Linear Mechanics
3 publications · 102 citations
3
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- ODU Digital Commons (Old Dominion University)
Repository · 2 publications · 52 citations
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