Effect of Fuselage and Wind Tunnel Wall on Full-Scale UH-60A Rotor Tip Vortex Prediction-Reference-Cited by-同舟云学术

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Effect of Fuselage and Wind Tunnel Wall on Full-Scale UH-60A Rotor Tip Vortex Prediction

Published:2016-06-10 Issue: Volume: Page:
ISSN:
Container-title:34th AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Jayaraman Buvaneswari¹,Potsdam Mark²

Affiliation:

1. Science and Technology Corporation

2. U.S. Army ADD

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3131

Reference16 articles.

1. Airloads Correlation of the UH-60A Rotor inside the 40- by 80-Foot Wind Tunnel

2. Comparison of Computed and Measured Vortex Evolution for a UH-60A Rotor in Forward Flight

3. Modular Multisolver Approach for Efficient High-Fidelity Simulation of the HART II Rotor

Cited by 1 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. Tip-Vortex Investigation on a Rotating and Pitching Rotor Blade;Journal of Aircraft;2018-09

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