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空间桁架动力弹塑性计算缩减方法精度分析

Precision Analysis of Elastoplastic Dynamic Reduction Method of the Space Trusses
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摘要 应用Newmark方法编制了空间网架动力弹塑性动力响应分析程序;改进并得出了一种动力缩减方法──考虑静残余的荷载相关Ritz矢量方法,编制了相应的弹塑性动力响应分析程序;为了检验缩减方法(Lcad-dependentRitzVectorsNewmark)的计算精度。用2种方法对同一空间桁架结构进行了计算,结果表明缩减方法具有较好的精度和可靠性。 In this paper, based on Newmark method, an elastoplastic dynamic analysis software for space truss structures was developed first. Then,to improve the efficiency of the analysis process, a dynamic reduction method- Load - dependent Ritz Vectors has been introduced into the calculation of the elastoplastic dynamic response in which the static residuces were considered. The iterative procedure has been presented and a new program has been developed. To test the precision of the new method,a space truss has been computed in comparision with the Newmark method. The results show that this Load -depentent Ritz Vectors Newmark method is good in efficiency and has high precision and reliability at the same time.
出处 《河北农业大学学报》 CAS CSCD 北大核心 1997年第2期93-98,共6页 Journal of Hebei Agricultural University
关键词 桁架 空间桁架 动力弹塑性 缩减法 Space truss Elastoplastics Reduction method
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参考文献3

  • 1何洪明,第四届全国结构工程学术会议论文集,1995年
  • 2姜晋庆,结构弹塑性有限元分析法,1990年
  • 3欧文 D R J,塑性力学有限元理论与应用,1989年,12页

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