首页 | 本学科首页   官方微博 | 高级检索  
     检索      

评述B—P统一弹—粘塑性本构模型
引用本文:宋迎东,高德平.评述B—P统一弹—粘塑性本构模型[J].南京航空航天大学学报,1997,29(5):593-599.
作者姓名:宋迎东  高德平
作者单位:南京航空航天大学动力工程系
摘    要:综述了Bodner-Partom统一弹-粘塑性本构模型的基本理论,包括流动法则、运动方程和内变量演变方程三个部分。该模型是基于位错动力学的思想提出来的,认为材料变形的应变率由弹性和非弹性两部分组成,它们始终耦合在一起,采用内变量来表示材料抵抗塑性变形的非弹性状态,内变量包括各向同性硬化和方向性硬化两种。该模型不需要屈服准则和加卸载准则,具有较强的模拟能力,能模拟循环硬化与循环软化、非比例加载引起的

关 键 词:粘塑性  本构方程  高温材料  航空发动机

A Review of B P Unified Elastic Viscoplastic Constitutive Model
Song Yingdong,Gao Deping.A Review of B P Unified Elastic Viscoplastic Constitutive Model[J].Journal of Nanjing University of Aeronautics & Astronautics,1997,29(5):593-599.
Authors:Song Yingdong  Gao Deping
Abstract:Summarizes the Bodner Partom unified elastic viscoplastic constitutive equations, including three parts,such as the flow laws, the kinetic equation and the evolution equations of internal variables. The model is developed from dislocation dynamics. The total strain rate is assumed to be composed of elastic and plastic components, which are coupled under all loading and unloading conditions. The inelastic state is expressed by internal variables. Yield criterion and loading and unloading criterion are not required in this model. Bodner Partom model can simulate the cyclic hardening or softening,additional hardening due to non proportional loading, thermal recovery, temperature dependence, damage development and so on. The paper also comments on the temperature dependence of the material constants. Finally the application of the model on aeroengine superalloys is introduced and the prospect of this model is predicted.
Keywords:viscoplasticity  constitutive equations  high  temperature materials  aeroengine  
本文献已被 CNKI 维普 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号