Blade Flapping Dynamics
Blade Flapping Dynamics is a rotorcraft flight mechanics phenomenon characterized by the vertical out-of-plane motion of rotor blades about a flapping hinge or equivalent structural compliance, enabling the blade to respond to aerodynamic and inertial forces arising from asymmetric inflow, cyclic pitch, and forward flight conditions.
113
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3.9K
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227
Authors
90
Institutions
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2017–2026
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Washington University in St. Louis
St Louis, United States
8 h-index
12 publications
278 citations
University of Maryland, College Park
College Park, United States
6 h-index
11 publications
323 citations
Massachusetts Institute of Technology
Cambridge, United States
5 h-index
8 publications
480 citations

Indian Institute of Science Bangalore
Bengaluru, India
3 h-index
7 publications
186 citations
Lockheed Martin (United States)
Bethesda, United States
3 h-index
5 publications
122 citations
University of California, Los Angeles
Los Angeles, United States
3 h-index
4 publications
69 citations
Technical University of Denmark
Kongens Lyngby, Denmark
3 h-index
6 publications
170 citations

Langley Research Center
Hampton, United States
3 h-index
3 publications
46 citations
1–8 of 90
14 publications · 501 citations
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5 publications · 81 citations
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5 publications · 131 citations
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Repository · 5 publications · 108 citations
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JSV · 5 publications · 133 citations
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