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西北工业大学 国内
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Damage tolerance properties of 2198-T8 integral fuselage panel between double friction stir weld joints
Yu E. Ma
, Bao Qi Liu, Zhen Qiang Zhao
航空学院
Northwestern Polytechnical University Xian
科研成果
:
书/报告/会议事项章节
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会议稿件
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同行评审
5
引用 (Scopus)
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探究 'Damage tolerance properties of 2198-T8 integral fuselage panel between double friction stir weld joints' 的科研主题。它们共同构成独一无二的指纹。
分类
加权
按字母排序
Engineering
Joints (Structural Components)
100%
Weld
100%
Damage Tolerance
100%
Residual Stress
25%
Crack Growth Rate
25%
Parent Material
25%
Mechanical Fatigue Test
12%
Stress-Intensity Factor
12%
Test Sample
12%
Experimental Finding
12%
Crack Grows
12%
Virtual Crack-Closure Technique
12%
Material Science
Residual Stress
100%
Damage Tolerance
100%
Crack Growth
100%
Stress Intensity Factor
50%
Aluminum-Lithium Alloys
50%
Crack Closure
50%