Flow Measurements and Multiple Pure Tone Noise From a Forward Swept Fan-Reference-Cited by-同舟云学术

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Flow Measurements and Multiple Pure Tone Noise From a Forward Swept Fan

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Weir Donald¹,Podboy Gary²

Affiliation:

1. Honeywell Engines

2. NASA Glenn

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1200

Reference6 articles.

1. Repp, R., Gentile, D., Hanson, D., and Chunduru, S. "Design and Test of Fan/Nacelle Models Quiet High-Speed Fan Design," NASA CR-2003-212369,2003.

2. Weir, D.S. "Design and Test of Fan/Nacelle Models, Quiet High-Speed Fan," NASA CR-2003-212370,2003.

3. Dittmar, J.H., Elliott, D.M., and Fite, E.B. "The Noise of a Forward Swept Fan," NASA TM-2003-212208,2003.

Cited by 4 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. Multiple Pure Tone Noise Predictions of a Propulsion Engine Fan with PowerFLOW;AIAA AVIATION 2023 Forum;2023-06-08

2. Effects of “S”-Type Bowed Guide Vanes on Unsteady Flow in 1.5-Stage Axial Compressors;Applied Sciences;2023-04-18

3. Effects of stator blade camber and surface viscosity on unsteady flow in axial turbine;Applied Thermal Engineering;2017-05

4. NASA Glenn’s Contributions to Aircraft Engine Noise Research;Journal of Aerospace Engineering;2013-04

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