IMECH-IR  > 力学所知识产出(1956-2008)
2024T3铝板试件疲劳裂纹张开应力测量
伍义生
Source Publication航空学报
1994-03-15
Issue03Pages:340-343
ISSN2000-6890
Abstract建立了一种用裂纹张开位移引伸计对2024T3铝板试件的疲劳裂纹张开应力进行自动测量的方法。比较了斜率法、切线相交法和切点法所得结果的差别及测点位置的影响。并给出了超载作用下的疲劳裂纹张开应力的测量结果。
Keyword疲劳 裂纹闭合 超载
Indexed ByCSCD
Language中文
CSCD IDCSCD:239292
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Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/72280
Collection力学所知识产出(1956-2008)
Recommended Citation
GB/T 7714
伍义生. 2024T3铝板试件疲劳裂纹张开应力测量[J]. 航空学报,1994(03):340-343.
APA 伍义生.(1994).2024T3铝板试件疲劳裂纹张开应力测量.航空学报(03),340-343.
MLA 伍义生."2024T3铝板试件疲劳裂纹张开应力测量".航空学报 .03(1994):340-343.
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