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高超声速湍流直接数值模拟技术
引用本文:李新亮.高超声速湍流直接数值模拟技术[J].航空学报,2015,36(1):147-158.
作者姓名:李新亮
作者单位:中国科学院力学研究所 高温气体动力学国家重点实验室, 北京 100190
基金项目:国家自然科学基金,国家“863”计划,中国科学院知识创新工程(KJCX2-EW-J01;XXH12503-02-02-04)National Natural Science Foundation of China,National High Technology Research and Development Program,Chinese Academy of Sciences Innovation Programs
摘    要:概述了近年来国内外高超声速湍流直接数值模拟(DNS)技术方面最新的研究进展,主要集中在高精度、高鲁棒性数值方法方面,同时也介绍了近年来典型的高超声速湍流DNS算例。在数值方法方面,主要介绍了高精度激波捕捉格式以及保持计算稳定的数值技术,重点是WENO格式及高阶保单调格式的最新进展。在高超声速湍流DNS算例方面,介绍了压缩性影响、壁温影响、真实气体效应以及高超声速转捩等方面的DNS研究。此外,还简要介绍了作者开发的可压缩高精度计算流体力学软件OpenCFD。

关 键 词:高超声速  湍流  直接数值模拟  高精度数值方法  OpenCFD

Direct numerical simulation techniques for hypersonic turbulent flows
LI Xinliang.Direct numerical simulation techniques for hypersonic turbulent flows[J].Acta Aeronautica et Astronautica Sinica,2015,36(1):147-158.
Authors:LI Xinliang
Institution:State Key Laboratory of High-temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190, China
Abstract:The recent developments of high resolution schemes, especially, high-order and high-robustness shock-capture schemes, and direct numerical simulation (DNS) cases for hypersonic turbulent flows are reviewed in this paper. The numerical methods include the high-resolution shock-capture methods and the technique to stabilize computation for hypersonic flows, as well as, the developments of WENO and monotonicity preserving schemes. The DNS studies include the effects of compressibility, wall temperature and high-temperature real gas on the turbulent flows, and the studies of hypersonic transition flows are also reviewed briefly. Furthermore, an OpenCFD code developed by the author which is compressible and high-resolution, is addressed briefly
Keywords:hypersonic  turbulence  direct  numerical  simulation  high-resolution  numerical  method  OpenCFD
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