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

燃气轮机叶轮非线性瞬态温度场的边界元分析
引用本文:姚寿广.燃气轮机叶轮非线性瞬态温度场的边界元分析[J].航空动力学报,1996,11(2):185-188.
作者姓名:姚寿广
作者单位:华东船舶工业学院
摘    要:首先采用克希荷夫变换将包含变物性及混合和辐射边界条件的热扩散方程转换成线性方程,进一步由加权余量法和离散化将方程转变成边界元方程组。用所开发的二维线性—非线性瞬态温度场边界元程序分析计算了燃气轮机叶轮起动工况下的非稳态温度场,与有限元数值计算结果比较表明,边界元法应用于这类非线性工程问题的分析是可靠、初始精度高,数值稳定性好及计算输入数据简单等优点。

关 键 词:燃气轮机  温度场  边界元法
收稿时间:3/1/1995 12:00:00 AM
修稿时间:8/1/1995 12:00:00 AM

ANALYSIS OF NONLINEAR TRANSIENT TEMPERATURE FIELD IN A GAS TURBINE DISC WITH BEM
Yao Shouguang.ANALYSIS OF NONLINEAR TRANSIENT TEMPERATURE FIELD IN A GAS TURBINE DISC WITH BEM[J].Journal of Aerospace Power,1996,11(2):185-188.
Authors:Yao Shouguang
Abstract:Kirchhoff's transform is employed to convert time dependent heat conduction equations,involving varying material properties and as well as radiation boundary condictions,into linear ones.Then the weighted residual method and discretization transform them into boundary element equations.On this basis,a 2-D linear/nonlinear transient temperature field analysis program has been set up to calculate the unsteady temperature field of a gas turbine disc in the starting regime.As compared with numerical results calculated with FEM,the results obtained show that the BEM method is reliable,and has many advantages,such as good initial accuracy and numerical stability,simplicity of input data preparation.Therefore,BEM is a very ideal numerical tool for analyzing gas turbine thermal problems.
Keywords:Gasturbines  Temperature field boundary element method
本文献已被 CNKI 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》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