
天津大学 机械工程学院,天津,300072
Published:2023
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黄章峰, 张宇琦. 高超声速三维边界层转捩数值研究进展及预测软件[J]. 空气动力学学报, 2023, 41(11): 1−19.
HUANG Zhangfeng, ZHANG Yuqi. Numerical research progress and prediction software of transition in hypersonic three-dimensional boundary layer[J]. 2023, 41(11): 1-19.
黄章峰, 张宇琦. 高超声速三维边界层转捩数值研究进展及预测软件[J]. 空气动力学学报, 2023, 41(11): 1−19. DOI: 10.7638/kqdlxxb-2023.0014
HUANG Zhangfeng, ZHANG Yuqi. Numerical research progress and prediction software of transition in hypersonic three-dimensional boundary layer[J]. 2023, 41(11): 1-19. DOI: 10.7638/kqdlxxb-2023.0014.
高超声速边界层转捩问题已经成为飞行器设计需要考虑的一个关键因素,也是高超声速流动研究的热点和难点。三维边界层中存在横流、流向涡、接触线三种典型的流动结构和失稳特征,他们诱导转捩的机理不同。本文总结了低雷诺数湍流、
γ-Re
θt
、
k-ω-γ
、层流动能4种常用转捩模型的构造、适用性及应用情况,介绍了适用于三维边界层的BiGlobal、PSE3D、TriGlobal三种全局稳定性分析方法,分析了基于转捩预测e
N
方法的eMalik、LASTRAC、LILO、HyTEN等转捩软件的优缺点,展望了高超声速三维边界层转捩研究及软件开发的未来。
Hypersonic boundary layer transition has become a key factor to be considered in aircraft design
and is also a hot and difficult point in hypersonic flow research. There are three typical flow structures and instability characteristics in hypersonic three-dimensional boundary layer
namely cross flow
flow direction vortex and contact line
which have different mechanisms to induce transition. Three global stability analysis methods (BiGlobal
PSE3D and TriGlobal) suitable for three-dimensional boundary layer are introduced. The structure
applicability and application of four commonly used transition models
such as the Low-Reynolds-Number turbulence model
γ-Re
θt
k-ω-γ
laminar-kinetic energy transition model
are summarized. The advantages and disadvantages of eMalik
LASTRAC
LILO
HyTEN and other transition softwares based on e
N
method are analyzed. The future of transition research and software development in hypersonic three-dimensional boundary layer is prospected.
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