Flutter Boundary Prediction is a computational or analytical method that identifies the critical flow velocity and frequency conditions at which aeroelastic instability arises in flexible structures, distinguishing itself by enabling the anticipation of flutter onset in nonlinear aerodynamic environments.
78
Publications
2.5K
Citations
194
Authors
87
Institutions
Publications per year
2017–2026
14
Parents
Publications
78
1–5 of 78
Authors
194
- MV
4
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- HT
4
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- MW
3
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- KJ
3
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- PB
3
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1–5 of 194
Institutions
87
Langley Research Center
Hampton, United States
8 h-index
13 publications
679 citations
Imperial College London
London, United Kingdom
5 h-index
11 publications
315 citations
Meijo University
Nagoya, Japan
4 h-index
4 publications
70 citations
ZONA Technology (United States)
Scottsdale, United States
4 h-index
8 publications
418 citations
Massachusetts Institute of Technology
Cambridge, United States
3 h-index
10 publications
255 citations
Beihang University
Beijing, China
3 h-index
8 publications
188 citations
University of Bristol
Bristol, United Kingdom
3 h-index
7 publications
172 citations
Rolls-Royce (United Kingdom)
London, United Kingdom
3 h-index
5 publications
198 citations
1–8 of 87
Venues
- AIAA Journal
14 publications · 445 citations
13
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- Journal of Aircraft
13 publications · 674 citations
12
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- Journal of Guidance Control and Dynamics
3 publications · 75 citations
3
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- Journal of Turbomachinery
3 publications · 119 citations
3
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- Journal of Fluids and Structures
3 publications · 68 citations
3
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