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Aeronautical Manufacturing Technology
2015
,
Issue (20)
: 69-72
DOI
: 10.16080/j.issn1671-833x.2015.20.069
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http://www.amte.net.cn/EN/10.16080/j.issn1671-833x.2015.20.069
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http://www.amte.net.cn/EN/Y2015/V58/I20/69
[1] 《中国航空材料手册》编辑委员会.钛合金铜合金(第4卷).北京：中国标准出版社， 2002.
[2] 郝传勇，李正林，毛先锋. Ti-55M高温Ti合金焊缝塑性的改善.金属学报，2001，37(7):709-712.
[3] 金蕾,李荻.钛合金化学铣切及电化学加工.稀有金属材料与工程，1989(2)：66-71.
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SUN Shouzheng,SUN Tianfeng,CHEN Weiqiang, FAN Dongxing,HAN Zhenyu,FU Hongya.
Load-Bearing Performance and Structure Optimization for Kagome Grid Satellite Cylinder Made by Filament Winding
[J]. Aeronautical Manufacturing Technology, 2021, 64(11): 34-40/49.
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Supported by:
Beijing Magtech
2015, Issue (20): 69-72 DOI: 10.16080/j.issn1671-833x.2015.20.069
