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用于可压缩自由剪切流动的湍流混合长度
引用本文:徐晶磊,宋友富,张扬,白俊强.用于可压缩自由剪切流动的湍流混合长度[J].航空学报,2016,37(6):1841-1850.
作者姓名:徐晶磊  宋友富  张扬  白俊强
作者单位:1. 北京航空航天大学 能源与动力工程学院, 北京 100083; 2. 西北工业大学 航空学院, 西安 710072
基金项目:航空发动机气动热力国家科技重点实验室基金(9140C410505150C41002)National Key Laboratory of Aircraft Engine Foundation of China (9140C410505150C41002)
摘    要:抓住可压缩流动变密度特性,构造出基于有效涡量的三维von Karman混合长度。湍流模型采用仅依赖湍动能k的单方程KDO(Kinetic Dependent Only)模型,引入新构造的混合长度替换旧尺度得到CKDO模型。为了验证其描述可压缩自由剪切湍流的能力,选择无壁面束缚、密度梯度大和可压缩效应强的自由剪切混合层为算例,其对流马赫数Mac=0.8。计算结果表明,KDO模型对混合层的速度分布有着良好的控制和模拟,而经可压缩修正后的CKDO模型与原模型及其他可压缩修正模型相比,所计算的速度分布、主雷诺剪切力和混合层厚度与试验结果更加接近,说明了该混合长度对可压缩混合层这种自由剪切湍流有着良好的刻画能力。

关 键 词:湍流模型  混合层  超声速流动  可压缩性  数值模拟  
收稿时间:2015-08-28
修稿时间:2015-11-04

Turbulence mixing length for compressible free shear flows
XU Jinglei,SONG Youfu,ZHANG Yang,BAI Junqiang.Turbulence mixing length for compressible free shear flows[J].Acta Aeronautica et Astronautica Sinica,2016,37(6):1841-1850.
Authors:XU Jinglei  SONG Youfu  ZHANG Yang  BAI Junqiang
Institution:1. School of Energy and Power Engineering, Beihang University, Beijing 100083, China; 2. School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China
Abstract:Seizing compressible flow variable density characteristics,a three-dimensional von Karman mixing length scale based on the effective vorticity has been constructed. This paper adopts a single-equation turbulence KDO (Kinetic Dependent Cnly) model which depends only on the turbulent kinetic energy equation, and introduces a new structure which replaces the old mixing length scale to obtain CKDO model. Then in order to verify its ability to describe compressible free shear turbulence, we select the compressible mixing layer of no wall bondage, large density gradient and strong compressibility effects as an example, whose convective Mach number is 0.8. The results show that KDO model has good control and simulation ability of mixing flow velocity distribution; compared with the original model and other compressible correction models, the velocity distribution, primary Reynolds shear stress and mixing layer thickness obtained with compressible correction model CKDO have a better fit with the experimental value. The results illustrate that the new mixing length has a good ability of characterization for compressible free shear turbulent mixing layer.
Keywords:turbulence model  mixing layer  supersonic flow  compressibility  numerical simulation
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