Blade-tip Vortex Interaction
Blade-Tip Vortex Interaction is a rotor aeroelastic phenomenon wherein the vortices shed from the tip of a rotating blade interact with subsequent blades or the blade itself, inducing unsteady aerodynamic loads and structural vibrations distinctive from other blade-vortex interactions due to the origin and trajectory of the tip-generated vortices.
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D. A. Boxwell, F. H. Schmitz, W. R. Splettstoesser et al. · Journal of the American Helicopter Society · 1987 · 86 citations · Full text
Engineering, Aerospace Engineering, Mechanical Engineering +16
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Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR), Germany
5 publications · 472 citations
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Ames Research Center
Mountain View, United States
12 h-index
25 publications
928 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
8 h-index
21 publications
1.2K citations

Langley Research Center
Hampton, United States
8 h-index
9 publications
183 citations
The Ohio State University
Columbus, United States
5 h-index
7 publications
189 citations

Nanjing University of Aeronautics and Astronautics
Nanjing, China
5 h-index
17 publications
269 citations
Massachusetts Institute of Technology
Cambridge, United States
5 h-index
9 publications
218 citations
United States Army
Arlington, United States
5 h-index
10 publications
297 citations

University of Glasgow
Glasgow, United Kingdom
4 h-index
7 publications
190 citations
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20 publications · 670 citations
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Repository · 8 publications · 134 citations
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