Supersonic Flutter Analysis is a computational and mathematical framework used in aeroelasticity to predict the onset of dynamic instability in aircraft structures subjected to supersonic airflow, distinguished by its integration of nonlinear aerodynamic forces, structural dynamics, and shock wave interactions specific to flight at speeds exceeding the speed of sound.
173
Publications
6.7K
Citations
332
Authors
168
Institutions
Publications per year
2017–2026
43
Parents
Publications
173
Nonlinear oscillations of a fluttering plate. II.
Earl H. Dowell · AIAA Journal · 1967 · 489 citations
1–5 of 173
Authors
332
- FL
6
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- ZS
5
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- SF
5
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- DH
4
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- VV
4
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1–5 of 332
Institutions
168
Purdue University West Lafayette
West Lafayette, United States
11 h-index
18 publications
747 citations
Harbin Institute of Technology
Harbin, China
10 h-index
24 publications
1.1K citations
Langley Research Center
Hampton, United States
10 h-index
13 publications
300 citations
Glenn Research Center
Cleveland, United States
7 h-index
8 publications
125 citations
Northwestern Polytechnical University
Xi'an, China
6 h-index
23 publications
916 citations
Beijing University of Technology
Beijing, China
6 h-index
12 publications
546 citations
Centre National de la Recherche Scientifique
Paris, France
6 h-index
11 publications
256 citations
Korea Advanced Institute of Science and Technology
Daejeon, South Korea
4 h-index
8 publications
232 citations
1–8 of 168
Venues
- AIAA Journal
26 publications · 1.6K citations
19
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- Composite Structures
21 publications · 1K citations
19
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- Journal of Aircraft
12 publications · 436 citations
11
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- Journal of Sound and Vibration
JSV · 9 publications · 381 citations
9
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- Aerospace Science and Technology
AST · 5 publications · 170 citations
4
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1–5