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	Rapid fabrication method of pre-research turbine blade wax precision mould based on 3D printing technology
	Lu, Zhongliang; Zhou, Jiangping; Yang, Dongsheng; Jing, Hui; Li, Dichen
刊名	Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
	2015
卷号	36期号:[db:dc_citation_issue]页码:651-660
关键词	Conformal cooling channels Cooling channels Gel casting Low surface roughness Manufacturing cycle Structure characteristic Temperature field distribution Turbine blade
ISSN号	1000-6893
DOI	[db:dc_identifier_doi]
URL标识	查看原文
WOS记录号	[DB:DC_IDENTIFIER_WOSID]
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/3266808
专题	西安交通大学
推荐引用方式 GB/T 7714	Lu, Zhongliang,Zhou, Jiangping,Yang, Dongsheng,et al. Rapid fabrication method of pre-research turbine blade wax precision mould based on 3D printing technology[J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,2015,36([db:dc_citation_issue]):651-660.
APA	Lu, Zhongliang,Zhou, Jiangping,Yang, Dongsheng,Jing, Hui,&Li, Dichen.(2015).Rapid fabrication method of pre-research turbine blade wax precision mould based on 3D printing technology.Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,36([db:dc_citation_issue]),651-660.
MLA	Lu, Zhongliang,et al."Rapid fabrication method of pre-research turbine blade wax precision mould based on 3D printing technology".Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica 36.[db:dc_citation_issue](2015):651-660.

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