Acoustic Effects of Liner Damage on Zero-Splice Turbofan Intake Liners: Computational Study
Author:
Affiliation:
1. Institute of Sound and Vibration Research, University of Southampton, Southampton, England SO17 1BJ, 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.J053219
Reference23 articles.
1. WatsonW. “Noise Suppression Characteristics of Peripherally Segmented Duct Liners,” NASA TP-1904, 1981.
2. Transmission in flow ducts with peripherally varying linings
3. Acoustic scattering by a spliced turbofan inlet duct liner at supersonic fan speeds
4. Discontinuous Galerkin Method for acoustic modes computation in lined ducts
5. A computational mode-matching approach for sound propagation in three-dimensional ducts with flow
Cited by 5 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. CFD/CAA coupling for the prediction of fan tone noise propagation and radiation through a drooped intake;28th AIAA/CEAS Aeroacoustics 2022 Conference;2022-06-13
2. Design of Tunable Acoustic Liner and Adaptive Control System;Acoustics Australia;2021-01-03
3. Modelling of boundary layer effects on the propagation of buzz-saw noise in lined ducts;25th AIAA/CEAS Aeroacoustics Conference;2019-05-18
4. Eigenmodes and Green's function of swirling flow in a duct with the lining varying circumferentially;23rd AIAA/CEAS Aeroacoustics Conference;2017-06-02
5. The Effect of Steady Flow Distortion on Noise Propagation in Turbofan Intakes;22nd AIAA/CEAS Aeroacoustics Conference;2016-05-27
1.学者识别学者识别
2.学术分析学术分析
3.人才评估人才评估
"同舟云学术"是以全球学者为主线，采集、加工和组织学术论文而形成的新型学术文献查询和分析系统，可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容，当前同舟云学术共收录了国内外主流学术期刊6万余种，收集的期刊论文及会议论文总量共计约1.5亿篇，并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询！咨询电话：010-8811{复制后删除}0370
www.globalauthorid.com
TOP
Copyright © 2019-2024 北京同舟云网络信息技术有限公司 京公网安备11010802033243号 京ICP备18003416号-3