Rotor Wake Study Near the Horizontal Tail of a T-Tail Configuration

Author:

Gorton Susan Althoff1,Berry John D.2,Hodges W. Todd3,Reis Deane G.3

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

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

1. Hub Flow Near-Wake Validation Using CREATETM-AV Helios and UMD Mercury Framework;Journal of the American Helicopter Society;2023-01-01

2. Full-Scale Reynolds Number Testing of Rotor Hub Drag and Wake Turbulence;Journal of the American Helicopter Society;2022-10-01

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

5. Flow field characterization and interactional aerodynamics analysis of a complete helicopter;Aerospace Science and Technology;2012-06

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