Flutter Boundary Determination
Flutter Boundary Determination is a methodological construct in aeroelastic testing that identifies the critical combination of flight conditions, such as airspeed and altitude, at which a structure transitions from stable oscillatory behavior to unstable, self-sustaining oscillations due to aerodynamic, elastic, and inertial coupling.
80
Publications
2.5K
Citations
196
Authors
85
Institutions
Publications per year
2017–2026
19
Parents
80
Calculation of Wing Flutter by a Coupled Fluid-Structure Method
F. Liu, Jianfeng Cai, Yanfei Zhu et al. · Journal of Aircraft · 2001 · 210 citations
Engineering, Aerospace Engineering, Computational Engineering +17
Some flutter solutions using finite elements
M. D. Olson · AIAA Journal · 1970 · 109 citations
1–5 of 80
196
United States Air Force Research Laboratory, United States
5 publications · 116 citations
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2
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1–5 of 196
85

Langley Research Center
Hampton, United States
7 h-index
18 publications
378 citations

Imperial College London
London, United Kingdom
5 h-index
11 publications
315 citations

Ames Research Center
Mountain View, United States
3 h-index
3 publications
63 citations
Massachusetts Institute of Technology
Cambridge, United States
3 h-index
8 publications
168 citations
Rolls-Royce (United Kingdom)
London, United Kingdom
3 h-index
5 publications
198 citations
ZONA Technology (United States)
Scottsdale, United States
3 h-index
5 publications
310 citations
The University of Texas at Austin
Austin, United States
3 h-index
4 publications
127 citations
Georgia Institute of Technology
Atlanta, United States
2 h-index
4 publications
67 citations
1–8 of 85
15 publications · 518 citations
12
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11 publications · 586 citations
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4 publications · 129 citations
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4 publications · 111 citations
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4 publications · 136 citations
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