A method of numerical modeling and parameter identification for a Kevlar laminate is proposed in this paper because of the complex mechanical behaviors and inaccurate parameters under the condition of hypervelocity impact. In the method. an orthotropic constitulive model, Chang-Chang failure model, and a finite element method are selected to describe the mechanical behaviors of Kevlar laminates; furthermore, the successive response surface technique is applied to identify the inaccurate parameters. Minimum least square residuals between simulation results and test results are taken as optimization objective. By using the method, eight numerical models for Al projeclile impacting Kevlar laminates, are modeled and the four parameters of failure criteria are identified. Numerical simulations have demonstrated the effectiveness of the proposed method.%针对Kevlar层合板在超高速撞击条件下的力学特性的复杂性及参数不准确对数值仿真的不利影响,提出一种使用正交各向异性本构模型,Chang-Chang复合材料失效模型和有限元方法对Kevlar层合板的超高速撞击力学特性进行建模并运用连续响应面技术对材料失效模型参数进行识别的方法.然后使用该方法建立了与现有文献中的试验工况相对应的数值模型,并把Kevlar层合板材料失效模型的4个参数作为优化变量,以仿真结果与试验结果的二乘残差最小作为优化目标,使用连续响应面技术建立参数优化模型,由此识别这些参数.结果表明,该建模方法能正确描述Kevlar层合板的超高速撞击力学特性,采用识别后的参数进行仿真计算可以显著提高数值模型的仿真精度.
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