The Structure of the Rotor Wake in Ground Effect-Reference-Cited by-同舟云学术

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The Structure of the Rotor Wake in Ground Effect

Published:2003-01-06 Issue: Volume: Page:
ISSN:
Container-title:41st Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Bhattacharyya Somnath¹,Conlisk A.¹

Affiliation:

1. Ohio State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-1255

Reference15 articles.

1. Tip Vortex Geometry of a Hovering Helicopter Rotor in Ground Effect

2. Light,J.S.

3. Modern helicopter rotor aerodynamics

4. Yeager, W.T., Jr., Young, W.H., Jr. and Mantay, W.H. "A Wind Tunnel Investigation of Parameters Affecting Helicopter Directional Control in GroundEffect", NASATN D-7694,Nov.1974.

Cited by 3 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. The Influence of Rotor Overlapping Azimuth on Compound Coaxial Helicopter Performance Based on Unsteady CFD Simulation;Applied Sciences;2023-01-06

2. Experimental and numerical examination of a helicopter hovering in ground effect;CEAS Aeronautical Journal;2013-07-25

3. Numerical Investigation of Helicopter Rotors in Ground Effect;30th AIAA Applied Aerodynamics Conference;2012-06-25

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