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

基于连续损伤模型的复合固体推进剂力学性能研究
引用本文:史佩,曲凯,张旭东.基于连续损伤模型的复合固体推进剂力学性能研究[J].海军航空工程学院学报,2010,25(6):662-666.
作者姓名:史佩  曲凯  张旭东
作者单位:[1]海军航空工程学院训练部,山东烟台264001 [2]海军航空工程学院飞行器工程系,山东烟台264001
摘    要:为了模拟复合固体推进剂本构关系,利用连续损伤力学理论并耦合线性累积损伤来建立含有损伤变量的本构模型。模型中推进剂累积损伤利用Miner线性累积损伤法则,损伤演化利用蠕变损伤演化规律,无损条件下的推进剂本构关系利用三元件波因廷模型。该模型提供了一种基于损伤本构关系来研究推进剂力学性能变化的有效方法。

关 键 词:推进剂  累积损伤  蠕变损伤  力学性能

Research on Mechanics Performance of Composite Propellant with Continuum Damage Mechanics
SHI Pei,QU Kai and ZHANG Xu-dong.Research on Mechanics Performance of Composite Propellant with Continuum Damage Mechanics[J].Journal of Naval Aeronautical Engineering Institute,2010,25(6):662-666.
Authors:SHI Pei  QU Kai and ZHANG Xu-dong
Institution:(Naval Aeronautical and Astronautical university a. Department of Training; b. Department of Airborne Vehicle Engineering, Yantai Shandong 264001, China)
Abstract:The methods of continuum damage mechanics can consistently incorporate existing propellant linear cumulative damage (LCD), which can better simulate the propellant constitutive behavior. The Miner's LCD models was applied in the model, the damage evolution law apply propellant creep damage evolution law. The viscoelastic material model with no damage uses Poynting model that is made up of three components. It provides a potential path to the coherent development of corresponding damage-based constitutive models.
Keywords:propellant  cumulative damage  creep damage  mechanics performance
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《海军航空工程学院学报》浏览原始摘要信息
点击此处可从《海军航空工程学院学报》下载免费的PDF全文
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