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Breakdown过程长度及其前后边界层名义厚度的变化
引用本文:唐洪涛.Breakdown过程长度及其前后边界层名义厚度的变化[J].航空动力学报,2008,23(5):810-815.
作者姓名:唐洪涛
作者单位:天津科技大学,机械工程学院,天津,300222;天津大学,力学系,天津,300072
基金项目:天津科技大学校科研和教改项目 , 国家自然科学基金
摘    要:采用数值模拟的方法,模拟了平板边界层的转捩过程及发展的湍流,在此基础上,研究了不同初始扰动对转捩持续时间和湍流边界层厚度影响的共性和差异.研究结果表明:在不同的波数情况下,计算得到不同的初始扰动引起的转捩的持续时间不同.在给定基本波数情况下,如果初始扰动在展向不是对称的,那么,它们引起的转捩后平均边界层厚度与转捩起始点处边界层厚度的比值δeb在相当长的时间内表现出相同的增长规律,这一增长规律与所加的初始扰动无关.然而,展向是非对称的表现出不同增长规律. 

关 键 词:航空、航天推进系统  转捩  湍流  波数  扰动
文章编号:1000-8055(2008)05-0810-06
收稿时间:2007/4/15 0:00:00
修稿时间:2007年4月15日

Durations of transition and variation of boundary-layer thickness before and after breakdown
TANG Hong-tao.Durations of transition and variation of boundary-layer thickness before and after breakdown[J].Journal of Aerospace Power,2008,23(5):810-815.
Authors:TANG Hong-tao
Institution:School of Mechanics Engineering, Tianjin University of Science and Technology, Tianjin 300222, China;Department of Mechanics, Tianjin University, Tianjin 300072, China
Abstract:Temporal mode direction numerical simulation has been done for the breakdown process of laminar-turbulent transition and the fully developed turbulence in an incompressible boundary layer on a flat plate.Based on the computational results,the common and different characteristics of the durations of transition and the time-averaged boundary-layer thickness induced by different initial disturbances were discussed.Analytical results show that under different basic wave numbers,the durations of transition induced by different initial disturbances are different to one another.On the other hand,under given basic wave numbers,if the initial disturbances are dissymmetrical in span-wise direction,the ratio of the time-averaged boundary-layer thickness after transition to the boundarylayer thickness at the beginning of the breakdown process in the transition,δeb,shows the same growth rate with respect to time,which is independent of the initial disturbances.In contrast,initial symmetric disturbances will induce different growth trends. 
Keywords:aerospace propulsion system  transition  turbulence  wave number  disturbance
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