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5A06铝合金的动态本构关系实验 被引量:27

Experimental investigation on a dynamic constitutive relationship of 5A06 Al alloy
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摘要 运用材料试验机和分离式霍普金森压杆装置(SHPB)对3种不同加工及热处理状态的5A06铝合金在常温~500℃、应变率为10^-4~10^3s^-1下的力学行为进行了实验研究。基于Johnson-Cook(JC)本构模型,通过实验数据拟合得到了每种状态下材料的本构模型参量。对Johnson-Cook本构模型中的应变率强化项作了修正,修正后的Johnson-Cook本构模型与实验数据基本吻合,从而确立了3种状态下5A06铝合金的动态本构关系。 Dynamic mechanical behaviors of 5A06 Al alloy by three kinds of processes and heat treatments were studied with the split Hopkinson pressure bar (SHPB) and static material test system over a wide range of strain rates and temperature. The Johnson-Cook constitutive relationship parameters were determined through these experiments. The strain-rate hardening term in the Johnson-Cook constitutive model was modified. The modified Johnson-Cook constitutive model is in agreement with the experimental data for 5A06 Al alloy.
出处 《爆炸与冲击》 EI CAS CSCD 北大核心 2009年第3期306-311,共6页 Explosion and Shock Waves
基金 国家空间碎片专题研究基金项目(kjsp06211)
关键词 固体力学 动态本构关系 霍普金森压杆 5A06铝合金 Johnson-Cook本构模型 solid mechanics dynamic constitutive relationship SHPB 5A06 A1 alloy Johnson-Cook model
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  • 1刘宗德,丰树平,张宁,韩铭宝,孙承纬.三种合金在短时高温下的热软化研究[J].爆炸与冲击,1996,16(2):97-104. 被引量:10
  • 2李宝山.国外热疲劳测试设备[A]..全国第四届热疲劳学术会议论文集[C].武汉:中国金属学会理化检验学会,1993.196~199.
  • 3[2]Christiansen E L,Kerr J H.Ballistics limit equations for spacecraft shielding[J].Int.J.Impact Engineering,2001,26:93~104.
  • 4[6]Palmieri D,Faraud M,Destefanis R.Whipple shied ballistic at impact velocity higher than 7km/s[J].Int.J.Impact Engineering,2001,26:579~590.
  • 5[7]Christiansen E L.Design and performance equation for advanced meteoroid and debris shields[J].Int.J.Impact Engineering,1993,14:145~156.
  • 6Bartolotta P A. Thermal - mechanical fatigue behavior of SiC / Ti24All 1Nb in air and argon environments[ J]. NASN -TM -105723, 1992, 28(8): 16-20.
  • 7Moreau D. Environment specification for quali - fication and acceptance of flight equipment[A]. 15^th aerospace testing saminar [C]. 1994.251-260.
  • 8Anfimov N . Part of testing in development of spaeaerafts and launch vehicles, russian ppro-aehes and experience [ A ]. 15^th aerospace testing seminar[C]. 1994.11 -22.
  • 9Shi H J, Pluvinage G. Cyclic stress - strain response during isothermal and thermal mechanical fatigue[J]. International Journal of Fatigue, 1994,16:549 -557.
  • 10马图哈KH.非铁合金的结构与性能[M].北京:科学出版社,1999.120-121.

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