Flight Dynamic Coupling
Flight Dynamic Coupling is a rotor aeroelastic phenomenon in which the dynamic response of the rotor blades interacts with the rigid-body flight dynamics of the aircraft, leading to mutually influencing oscillatory modes that can alter stability, control, and handling characteristics.
16
Publications
518
Citations
46
Authors
23
Institutions
Publications per year
2017–2026
3
Parents
16
1–5 of 16
46
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23

Ames Research Center
Mountain View, United States
4 h-index
6 publications
113 citations
Georgia Institute of Technology
Atlanta, United States
3 h-index
5 publications
213 citations

DEVCOM Army Research Laboratory
Adelphi, United States
2 h-index
2 publications
44 citations
Stinger Ghaffarian Technologies (United States)
Greenbelt, United States
1 h-index
3 publications
48 citations
Airbus (United Kingdom)
Bristol, United Kingdom
1 h-index
6 publications
276 citations

Pennsylvania State University
State College, United States
1 h-index
4 publications
80 citations

Universitat Autònoma de Barcelona
Cerdanyola del Vallès, Spain
1 h-index
1 publications
52 citations

Langley Research Center
Hampton, United States
1 h-index
1 publications
20 citations
1–8 of 23
4 publications · 113 citations
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Conference · 2 publications · 41 citations
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1 publications · 17 citations
1
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Conference · 1 publications · 13 citations
1
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1 publications · 114 citations
1
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1–5