The Effect of Dynamic Stall on the Response and Airloading of Helicopter Rotor Blades
Author:
Affiliation:
1. Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, Massachusetts 02139
Publisher
American Helicopter Society
Cited by 15 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
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4. Development of Modal Analysis Based Clustering Technique Using Pitching Airfoil Measurements;AIAA Scitech 2019 Forum;2019-01-06
5. Analysis of Dynamic Stall Using Dynamic Mode Decomposition Technique;AIAA Journal;2014-11
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