首页 | 本学科首页   官方微博 | 高级检索  
     

可压缩非平行流边界层稳定性研究
引用本文:唐登斌,马前容,成国玮. 可压缩非平行流边界层稳定性研究[J]. 航空学报, 2002, 23(2): 166-169
作者姓名:唐登斌  马前容  成国玮
作者单位:南京航空航天大学,空气动力学系,江苏,南京,210016
基金项目:航空基础科学基金资助项目 (94A5 2 0 13 )
摘    要: 采用线性稳定性理论和多重尺度方法,研究三维可压缩的非平行流边界层稳定性问题。分析了可解条件的特征,导出精确计算所需的伴随问题方程渐近外边界条件的矩阵表达式,给出有控制的重正化方法,以有效地克服刚性方程在积分求解中的困难。探讨与非平行性作用相关的方程和影响因素,特别是新的特征函数畸变对扰动增加率的作用。通过算例,清楚地显示了流动的非平行性对边界层稳定性的影响。

关 键 词:非平行流  边界层稳定性  三维  可压缩流  多重尺度法  
文章编号:1000-6893(2002)02-0166-04
修稿时间:2001-02-13

STUDY OF COMPRESSIBLE NONPARALLEL FLOW STABILITY FOR BOUNDARY LAYERS
TANG Deng-bin,MA Qian-rong,CHEN Guo-wei. STUDY OF COMPRESSIBLE NONPARALLEL FLOW STABILITY FOR BOUNDARY LAYERS[J]. Acta Aeronautica et Astronautica Sinica, 2002, 23(2): 166-169
Authors:TANG Deng-bin  MA Qian-rong  CHEN Guo-wei
Affiliation:Department of Aerodynamics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:WT5”BZ]The compressible linear stability theory and the method of multiple scales are used to study the problem of three dimensional nonparallel flow stability for boundary layers. Solvability condition is analyzed. A matrix expression of the asymptotic edge boundary condition, which is used to exact numerical computation, is derived. A controlled renormalization method is used, in order to resolve the difficulty due to the stiff feature of these equations. The related equations and elements to nonparallelism are studied, including specifically the effect of new distortion of the eigenfunction on the disturbance growth rate which is important for boundary layer stability. The examples presented clearly show the effect of nonparallel flow on boundary layer stability.
Keywords:nonparallel flow  boundary layer stability  three dimensions  compressible flow  multiple scales method
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载全文
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