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	Design of locally reacting liner based on transfer element method and experimental validation [基于传递单元方法的局域反应声衬设计与试验]
	Li, Z.; Wang, X.; Sun, X.
刊名	Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
	2018
卷号	39
关键词	Acoustic impedance Acoustic noise Aircraft engines Axial flow turbomachinery Axial-flow compressors Cost engineering Ducts Engines Wave transmission Axial compressors Engineering applications Experimental validations Locally reacting liner Low speed axial compressor Noise reduction effect Transfer elements Transmission loss Noise abatement
ISSN号	10006893
DOI	10.7527/S1000-6893.2018.22053
URL标识	查看原文
收录类别	CSCD
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5928813
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Li, Z.,Wang, X.,Sun, X.. Design of locally reacting liner based on transfer element method and experimental validation [基于传递单元方法的局域反应声衬设计与试验][J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,2018,39.
APA	Li, Z.,Wang, X.,&Sun, X..(2018).Design of locally reacting liner based on transfer element method and experimental validation [基于传递单元方法的局域反应声衬设计与试验].Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,39.
MLA	Li, Z.,et al."Design of locally reacting liner based on transfer element method and experimental validation [基于传递单元方法的局域反应声衬设计与试验]".Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica 39(2018).

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