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Aeronautical Manufacturing Technology
2015
,
Issue (8)
: 92-94
DOI
: 10.16080/j.issn1671-833x.2015.08.092
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http://www.amte.net.cn/EN/10.16080/j.issn1671-833x.2015.08.092
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http://www.amte.net.cn/EN/Y2015/V58/I8/92
[1] 理有亲．钛板冲压成形技术．北京：国防工业出版社．1986.
[2] 李鹏亮．钛合金热成形模具. 航空制造技术，2012(21)：94-97.
[3] 林尧．TC4钛合金框类零件热挤压数值模拟及工艺优化. 宇航材料工艺，2010(3)：26-29.
[4] 陈淳,陆辰,张东升.航空发动机钛合金板材热成形加工技术//2008年中国航空学会制造工程分会学术会议论文集.2008.
[5] 蒋骏．钛合金零件制造技术．北京：国防工业出版社，1991.
[1]
YANG Haibo，ZHU Bo，GAO Xingqiang，LEI Yu.
Effects of Penetrating Holes on Tensile Properties of Titanium Honeycomb Core Panels With Variable Cross-Section
[J]. Aeronautical Manufacturing Technology, 2022, 65(3): 92-95/100.
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Beijing Magtech
2015, 
