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采用近似边界求解壁板颤振的CBS有限元算法
引用本文:李凯伦,魏云,张玫琳,张家忠.采用近似边界求解壁板颤振的CBS有限元算法[J].航空动力学报,2015,30(12):2848-2856.
作者姓名:李凯伦  魏云  张玫琳  张家忠
作者单位:1. 西安交通大学能源与动力工程学院, 西安 710049;
基金项目:国家重点基础研究发展计划(2012CB026002);国家科技支撑计划(2013BAF01B02)
摘    要:为了简化Euler方程求解壁板颤振问题,将近似边界条件成功地推广到CBS(characteristic-based split)有限元方法求解壁板颤振领域,把运动壁面的影响转化为Euler方程的边界条件,避免了对动网格的处理.通过对近似边界方法、动网格方法以及3阶活塞理论的数值模拟结果进行对比发现:首先,加载近似边界的CBS有限元方法操作非常简便,且模拟结果与动网格方法完全吻合;其次,Euler方程可以准确捕捉到壁板前后两端不光滑尖点所引起的压力突跳,而3阶活塞理论则无法做到;最后,采用近似边界的CBS有限元方法在求解无黏可压缩流动中细长体小变形的流-固耦合问题上具有潜力和优势. 

关 键 词:壁板颤振    流-固耦合    CBS有限元算法    近似边界条件    动网格
收稿时间:2014/4/27 0:00:00

CBS finite element method with approximate boundary conditions for panel flutter
LI Kai-lun,WEI Yun,ZHANG Mei-lin and ZHANG Jia-zhong.CBS finite element method with approximate boundary conditions for panel flutter[J].Journal of Aerospace Power,2015,30(12):2848-2856.
Authors:LI Kai-lun  WEI Yun  ZHANG Mei-lin and ZHANG Jia-zhong
Institution:1. School of Energy and Power Engineering, Xi'an Jiaotong University, Xi'an 710049, China;2. Boiler and Enviromental Protection Department, Xi'an Thermal Power Research Institute Company Limited, Xi'an 710032, China;3. Henan Electric Power Survey and Design Institute, Power Construction Corporation of China, Zhengzhou 450007, China
Abstract:In order to simplify the solving process of Euler equation for panel flutter, approximate boundary conditions were successfully introduced into CBS (characteristic-based split) finite element method to simulate the panel flutter. The impact of moving boundary was treated as normal boundary conditions for Euler equation. From analysis, it is found that:first, the results by approximate boundary conditions agree very well with those by moving boundary method, and the application of approximate boundary conditions is more convenient; then, Euler equation, rather than 3rd order piston theory is able to capture the pressure jump caused by sharp points at the ends of panels; finally, CBS finite element method with approximate boundary conditions has potentials and advantages in solving the fluid-structure interaction problems of small deformation of slender bodies in inviscid compressible flows.
Keywords:panel flutter  fluid-structure interaction  CBS finite element method  approximate boundry conditions  moving mesh
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