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高强度铝合金小裂纹疲劳扩展规律研究 被引量:1

PROPAGATING PROPERTIES OF SMALL CRACKS IN HIGH STRENGTH ALUMINUM
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摘要 考虑了高强度铝合金表面局部塑性变形特点,并引入小裂纹尖端屈服应力的渐变规律.分析了裂纹尖端屈服应力的这种变动对裂纹张开应力变动规律的影响.同时它还与T应力共同作用使得线弹性断裂力学不再适用于预测小裂纹尖端塑性区.据此可以解释小裂纹扩展的规律。 Based on the surface local plastic deformation,the variation of crack tip yielding stress in small crack stages were introduced. Because of the lower level of the crack tip yielding stress corresponding to small crack stage,the opening stress of small crack will change from a lower level to its ordinary value.Besides ,the description of the crack propagation with two parameters (the SIF range and T stress term in the Williams series) can explain the fatigue properties of the small cracks,which shows that the propagation of the small cracks cannot be predicted within the scope of LEFM theory.
出处 《北京航空航天大学学报》 EI CAS CSCD 北大核心 1996年第3期274-278,共5页 Journal of Beijing University of Aeronautics and Astronautics
基金 国家自然科学基金
关键词 裂纹 疲劳 塑性变形 裂纹扩展 铝合金 crack fatigue plastic deformation crack propagation T stress
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同被引文献28

  • 1陈勃,吴学仁,刘建中.基于小裂纹扩展的耐久性分析和经济寿命预测方法[J].机械强度,2004,26(z1):246-249. 被引量:7
  • 2吴学仁,刘建中.基于小裂纹理论的航空材料疲劳全寿命预测[J].航空学报,2006,27(2):219-226. 被引量:47
  • 3丁传富,吴学仁.疲劳小裂纹的断裂力学参数及试验方法的研究进展[J].航空学报,1996,17(6):640-647. 被引量:11
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