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沿流向微结构沟槽流场直接数值模拟
引用本文:李超群,李易,张晨曦,唐硕.沿流向微结构沟槽流场直接数值模拟[J].航空学报,2020,41(11):123628-123628.
作者姓名:李超群  李易  张晨曦  唐硕
作者单位:1. 西北工业大学 航天学院, 西安 710072;2. 陕西省空天飞行器设计重点实验室, 西安 710072
摘    要:采用高阶格式对覆有V型对称沟槽表面的槽道湍流流动进行了直接数值模拟,数值方法采用有限差分法。为精确求解沟槽壁面的湍流流动,对流项的离散采用7阶WENO(Weighted Essentially Non-Oscillatory)格式;时间推进采用分数步时间推进与低耗散、低色散Runge-Kutta方法(LDDRK方法)结合的格式;黏性项的离散采用6阶中心格式。模拟的雷诺数为5 000(基于槽道高度的1/2),计算的沟槽宽度范围为13~44,沟槽斜壁与水平面夹角为60°。数值模拟结果表明,与平板相比,沿流向沟槽表面的阻力最高降低了9%。数据分析发现出现减阻效果时,沟槽减少了近壁面处顺流向涡的数目,并且减阻机理与微沟槽阻碍大尺度流向涡与沟槽壁面的直接碰撞,使沟槽表面湍流脉动得到削弱有关。

关 键 词:微结构沟槽  湍流减阻  不可压缩流动  直接数值模拟  有限差分法  高阶WENO格式  
收稿时间:2019-11-04
修稿时间:2019-11-20

Direct numerical simulation of flow field over streamwise micro riblets
LI Chaoqun,LI Yi,ZHANG Chenxi,TANG Shuo.Direct numerical simulation of flow field over streamwise micro riblets[J].Acta Aeronautica et Astronautica Sinica,2020,41(11):123628-123628.
Authors:LI Chaoqun  LI Yi  ZHANG Chenxi  TANG Shuo
Institution:1. School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China;2. Shaanxi Aerospace Flight Vehicle Design Key Laboratory, Xi'an 710072, China
Abstract:To simulate the flow over the streamwise micro riblets of symmetric V shape, this paper applies a model of channel flow where the lower wall is mounted with riblets and the upper one is flat. The finite difference method is employed as the numerical method. To accurately obtain the flow of riblets, the 7th WENO (Weighted Essentially Non-Oscillatory) scheme, the fractional-step method combined with the Low-Dissipation and Dispersion Runge-Kutta scheme (LDDRK method) and the 6th central scheme are applied to the discretization of the space, the time advancing and viscous terms. In this paper, the Reynolds number is 5 000 (based on the half width of the channel), the range of the size of the riblets is from 13 to 44 and the inclination of the slope of riblets is 60°. Simulation results illustrate that the maximum of drag reduction is 9% and indicate that in the drag-reducing cases, the riblets can prevent the large-scale streamwise vortices from interacting with the surface directly, weakening the turbulent oscillation and decreasing the number of the streamwise vortices near riblet wall.
Keywords:micro riblets  turbulent drag reduction  incompressible flow  direct numerical simulation  finite difference method  high-order WENO scheme  
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