Special Vortices at a Helicopter Rotor Blade-Reference-Cited by-同舟云学术

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Special Vortices at a Helicopter Rotor Blade

Published:1990-10-01 Issue:4 Volume:35 Page:16-22
ISSN:2161-6027
Container-title:Journal of the American Helicopter Society
language:en
Short-container-title:j am helicopter soc

Author:

Mu¨ller Reinert H. G.¹

Affiliation:

1. FIBUS Research Institute, Aachen, W. Germany

Publisher

American Helicopter Society

Cited by 14 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

1. Vacuum and Hover Tests of a Dihedral–Anhedral Tip Composite Rotor;Journal of Aircraft;2023-09

2. A new blade tip geometry to improve aerodynamic performance and acoustic noise of helicopter blade in hovering flight;Aerospace Science and Technology;2023-04

3. A review of helicopter rotor blade tip shapes;Progress in Aerospace Sciences;2013-01

4. Wake Effects of Free-Wake Model on Aeroelastic Behavior of Hovering Rotors;Journal of Aircraft;2011-07

5. Blade Vortex Interactions: Experimental Measurements of the Near-Flow Field;Journal of Fluid Science and Technology;2009

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