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	Quantitative analysis method of whole aero-engine structural design based on structural efficiency
	Peng, G.; Li, C.; Zheng, H.; Ma, Y.; Hong, J.
刊名	Mechanisms and Machine Science
	2019
卷号	63页码:3-17
关键词	Aircraft engines Bypass ratio Efficiency Gas turbines Machine design Structural design Aero gas turbine engines Aero-engine Evaluation parameters High bypass ratio turbo-fan engines Mechanical characteristics Performance improvements Structural efficiencies Structural systems Structural optimization
ISSN号	22110984
DOI	10.1007/978-3-319-99272-3_1
URL标识	查看原文
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5922592
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Peng, G.,Li, C.,Zheng, H.,et al. Quantitative analysis method of whole aero-engine structural design based on structural efficiency[J]. Mechanisms and Machine Science,2019,63:3-17.
APA	Peng, G.,Li, C.,Zheng, H.,Ma, Y.,&Hong, J..(2019).Quantitative analysis method of whole aero-engine structural design based on structural efficiency.Mechanisms and Machine Science,63,3-17.
MLA	Peng, G.,et al."Quantitative analysis method of whole aero-engine structural design based on structural efficiency".Mechanisms and Machine Science 63(2019):3-17.

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