Fatigue crack growth rate of aluminum alloys under Ⅰ-Ⅲ combined loading
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摘要: 通過有限元數值模擬和疲勞裂紋擴展試驗,研究了鋁合金材料在Ⅰ-Ⅲ復合型加載條件下的疲勞裂紋擴展規律,得到了在不同加載情況下裂紋的應力強度因子、裂紋前緣能量場和塑性區半徑.在分析Ⅰ型拉力載荷對裂紋擴展的基礎上,著重分析了Ⅲ型加載對Ⅰ型裂紋應力強度因子及裂紋前緣能量場的影響.結果表明:應力強度因子KⅠ隨著Ⅲ型加載的增大而減小,而裂紋附近塑性區半徑增大.進行Ⅲ型靜態加載會使疲勞裂紋擴展速率減小,在一定范圍內,Ⅰ-Ⅲ復合型疲勞裂紋擴展速率隨著Ⅲ型加載的增加而減小;而在進行Ⅲ型循環加載會使疲勞裂紋擴展速率增大,在一定范圍內,Ⅰ-Ⅲ復合型疲勞裂紋擴展速率隨著Ⅲ型加載的增加而增大.Abstract: Fatigue crack propagation laws of aluminum alloys under Ⅰ-Ⅲ combined loading were investigated by finite element simulation and fatigue crack growth experiment,and the stress intensity factors under various loading conditions,the energy field around the crack front and the radius of the plastic zone were obtained.The effects of mode Ⅲ loading on the energy field around the crack front and the stress intensity factor under mode Ⅰ loading were analyzed on the basis of studies on mode Ⅰ loading.Numerical results show that under the condition of Ⅰ-Ⅲ combined loading,the stress intensity factor decreases with the increasing of mode Ⅲ loading,but the radius of the plastic zone near the crack increases.Mode Ⅲ static loading can slow down fatigue crack propagation,and to some extent,the fatigue crack growth rate under combined Ⅰ-Ⅲ loading decreases with the increasing of mode Ⅲ static loading.Mode Ⅲ cyclic loading can speed up fatigue crack propagation,and to some extent,the fatigue crack growth rate under Ⅰ-Ⅲ combined loading increases with the increasing of mode Ⅲ loading.
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Key words:
- fatigue of materials /
- aluminum alloys /
- fatigue crack propagation /
- stress intensity factors /
- loading
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