Rotor Wake Study Near the Horizontal Tail of a T-Tail Configuration
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681-2199
2. U.S. Army Aviation and Missile Command, Redstone Arsenal, Alabama 35898-5000
3. U.S. Army Aviation and Missile Command, Hampton, Virginia 23681-2199
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2977
Reference48 articles.
Cited by 6 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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3. Visualization of a helicopter rotor hub wake;Experiments in Fluids;2018-06-22
4. A Review of 60 Years of Rotor Hub Drag and Wake Physics: 1954–2014;Journal of the American Helicopter Society;2016-04-01
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