Rotor Blade Flutter is a dynamic aeroelastic instability characterized by self-sustained, divergent oscillations of a rotor blade arising from the coupling between aerodynamic, inertial, and elastic forces under specific flight conditions.
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Glenn Research Center
Cleveland, United States
6 h-index
10 publications
240 citations
Northeastern University
Boston, United States
4 h-index
12 publications
419 citations
Duke University
Durham, United States
4 h-index
8 publications
332 citations
Purdue University West Lafayette
West Lafayette, United States
3 h-index
3 publications
57 citations
Hartford Financial Services (United States)
Hartford, United States
3 h-index
4 publications
88 citations
Technische Universität Darmstadt
Darmstadt, Germany
2 h-index
10 publications
210 citations
University of Florence
Florence, Italy
2 h-index
9 publications
100 citations
Instytut Techniczny Wojsk Lotniczych
Warsaw, Poland
2 h-index
3 publications
70 citations
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- Journal of the American Helicopter Society
10 publications · 344 citations
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- AIAA Journal
8 publications · 336 citations
8
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- Journal of Turbomachinery
5 publications · 180 citations
5
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- Journal of Sound and Vibration
JSV · 4 publications · 146 citations
4
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- Journal of Engineering for Gas Turbines and Power
4 publications · 426 citations
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