Optimization of Bypass Outlet Guide Vane for Low Interaction Noise-Reference-Cited by-同舟云学术

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Optimization of Bypass Outlet Guide Vane for Low Interaction Noise

Published:2014-06 Issue:6 Volume:52 Page:1145-1158
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Giacché Davide¹,Xu Liping¹,Coupland John²

Affiliation:

1. Department of Engineering, University of Cambridge, Cambridge, England CB3 0DY, United Kingdom

2. Rolls-Royce plc, Derby, England DE24 8BJ, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J052003

Reference27 articles.

1. JohnstonR. P. “Energy Efficient Engine—Preliminary Design and Integration Study,” NASA CR-135444, 1978.

2. Subsonic transport noise

3. Fan Noise Reduction: An Overview

4. HuffD. L. “Noise Reduction Technologies for Turbofan Engines,” NASA TM-2007-214495.

5. BolgerJ. J. “Three-Dimensional Design of Compressor Blades,” Ph.D. Thesis, Univ. of Cambridge, Cambridge, England, U.K. 1999.

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3. Radical Guide Vane Design and Optimization;Journal of Propulsion and Power;2018-11

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5. On the study of wavy leading-edge vanes to achieve low fan interaction noise;Journal of Sound and Vibration;2018-04

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