| 注册
首页|期刊导航|空气动力学学报|基于调和线性化Navier-Stokes方程的局部感受性

基于调和线性化Navier-Stokes方程的局部感受性

黄加昊 赵磊 赵瑞

空气动力学学报2024,Vol.42Issue(3):69-82,14.
空气动力学学报2024,Vol.42Issue(3):69-82,14.DOI:10.7638/kqdlxxb-2023.0068

基于调和线性化Navier-Stokes方程的局部感受性

Local receptivity based on harmonic linearized Navier-Stokes equations

黄加昊 1赵磊 2赵瑞3

作者信息

  • 1. 天津大学力学系,天津 300350
  • 2. 天津大学力学系,天津 300350||天津市现代工程力学重点实验室,天津 300350
  • 3. 北京理工大学宇航学院,北京 100081
  • 折叠

摘要

Abstract

The receptivity of Mack mode in the hypersonic boundary layer determines the initial amplitudes of disturbances that trigger transition.Therefore,considering the receptivity is a fundamental prerequisite for developing rational transition prediction methods.The excitation of Mack mode by the interaction between localized wall roughness and incoming acoustic waves is a typical local receptivity process,which can be generally described by three methods,i.e.,the large-Reynolds-number asymptotic theory,the finite-Reynolds-number theory,and direct numerical simulations.However,the first two theories become invalid under the condition of finite-height roughness due to the hypothesis of small(linear)roughness involved,whereas the third method is computationally intensive and not suitable for parametric study.In the present study,an efficient method for computing the local receptivity is developed based on the harmonic linearized Navier-Stokes equation(HLNS),and the local receptivity of Mack mode,induced by the interaction between the acoustic wave and the small/finite-height roughness,is systematically investigated in the hypersonic boundary layer at a Mach number of 5.92.The results suggest that the local receptivity of Mack mode induced by fast acoustic waves is significantly stronger than that of slow acoustic waves.For finite-height roughness,the local receptivity of fast acoustic waves shows a super-linear enhancement with the increase of roughness height within a large range of acoustic parameters.

关键词

感受性/粗糙元/调和线性化Navier-Stokes方程/高超声速边界层

Key words

receptivity/roughness/HLNS equations/hypersonic boundary layer

分类

航空航天

引用本文复制引用

黄加昊,赵磊,赵瑞..基于调和线性化Navier-Stokes方程的局部感受性[J].空气动力学学报,2024,42(3):69-82,14.

基金项目

国家自然科学基金青年基金(12002235) (12002235)

国家自然科学基金企业联合基金重点项目(U20B2003) (U20B2003)

空气动力学学报

OA北大核心CSTPCD

0258-1825

访问量0
|
下载量0
段落导航相关论文