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高超声速湍流直接数值模拟技术
Direct numerical simulation techniques for hypersonic turbulent flows

查看参考文献44篇

李新亮 *  
文摘 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。
其他语种文摘 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.
来源 航空学报 ,2015,36(1):147-158 【核心库】
DOI 10.7527/s1000-6893.2014.0233
关键词 高超声速 ; 湍流 ; 直接数值模拟 ; 高精度数值方法 ; OpenCFD
地址

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

语种 中文
文献类型 研究性论文
ISSN 1000-6893
学科 力学;航空
基金 中国科学院知识创新工程项目 ;  国家863计划 ;  国家自然科学基金
文献收藏号 CSCD:5346481

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引证文献 8

1 印智昭 基于高阶WENO格式的旋翼非定常涡流场数值模拟 航空学报,2016,37(8):2552-2564
被引 4

2 杨基明 激波的传播与干扰 力学进展,2016,46(1):541-587
被引 12

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