Flutter Onset is a critical dynamic instability phenomenon in aeroelasticity that constitutes the threshold at which an airfoil's coupled bending and torsional modes begin to exhibit self-sustained oscillations due to the interplay of inertial, elastic, and aerodynamic forces.
138
Publications
5.1K
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321
Authors
163
Institutions
Publications per year
2017–2026
43
Variants
Flutter Boundary
Parents
Publications
138
Proceedings of the National Academy of Sciences · 2005 · 304 citations · Full text
Frequency lock-in is caused by coupled-mode flutter
Emmanuel de Langre · Journal of Fluids and Structures · 2006 · 147 citations
Engineering, Physics, Vibration +10
1–5 of 138
Authors
321
- EH
8
h-index
- JT
6
h-index
- PBPhilip Beran
United States Air Force Research Laboratory, United States
5 publications · 120 citations
5
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- AV
5
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- RC
5
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1–5 of 321
Institutions
163
Duke University
Durham, United States
8 h-index
19 publications
540 citations
Langley Research Center
Hampton, United States
7 h-index
17 publications
343 citations
Universidad Politécnica de Madrid
Madrid, Spain
5 h-index
11 publications
178 citations
United States Air Force
Arlington, United States
5 h-index
7 publications
242 citations
Wright-Patterson Air Force Base
Wright-Patterson AFB, United States
5 h-index
9 publications
359 citations
U.S. Air Force Institute of Technology
Dayton, United States
4 h-index
6 publications
192 citations
University of Michigan
Ann Arbor, United States
4 h-index
7 publications
127 citations
University of Trento
Trento, Italy
4 h-index
10 publications
467 citations
1–8 of 163
Venues
- Journal of Aircraft
12 publications · 439 citations
12
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- AIAA Journal
11 publications · 327 citations
11
h-index
- Journal of Fluids and Structures
11 publications · 490 citations
11
h-index
- Journal of Sound and Vibration
JSV · 8 publications · 495 citations
8
h-index
- Journal of the Mechanics and Physics of Solids
5 publications · 231 citations
5
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1–5