高速高温湍流研究进展

袁先旭; 刘朋欣; 周清清; 傅亚陆; 杨肖峰; 杜雁霞

doi:10.7638/kqdlxxb-2023.0185

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高速高温湍流研究进展

研究综述 | 更新时间：2026-05-28

- 高速高温湍流研究进展
- Progress in high-speed high-temperature turbulence research
- 空气动力学学报 2024年42卷第4期页码：1-13
- 作者机构：
  
  空天飞行空气动力科学与技术全国重点实验室,绵阳,621000
- 作者简介：
  
  袁先旭（1974—），男，博士，研究方向：高速空气动力学. E-mail： yuanxianxu@skla.cardc.cn
  刘朋欣*（1990—），男，博士，研究方向：高温非平衡流动，湍流. E-mail：liupengxin@cardc.cn
- 基金信息：
  
  国家重点研发计划（2019YFA0405200）;国家自然科学基金（12272396）
- DOI：10.7638/kqdlxxb-2023.0185
  中图分类号： V211
- 纸质出版：2024
- 稿件说明：
移动端阅览
袁先旭, 刘朋欣, 周清清, 等. 高速高温湍流研究进展[J]. 空气动力学学报, 2024, 42(4): 1−13.

YUAN Xianxu, LIU Pengxin, ZHOU Qingqing, et al. Progress in high-speed high-temperature turbulence research[J]. 2024, 42(4): 1-13.
袁先旭, 刘朋欣, 周清清, 等. 高速高温湍流研究进展[J]. 空气动力学学报, 2024, 42(4): 1−13. DOI： 10.7638/kqdlxxb-2023.0185

YUAN Xianxu, LIU Pengxin, ZHOU Qingqing, et al. Progress in high-speed high-temperature turbulence research[J]. 2024, 42(4): 1-13. DOI： 10.7638/kqdlxxb-2023.0185.

摘要

低空域高速飞行条件下的飞行器表面边界层具有高马赫数、高雷诺数、高总焓的特点。较高的来流雷诺数使边界层发生从层流到湍流的转捩，而强激波压缩形成的高温环境将导致气体分子出现振动能激发、离解、电离等热化学非平衡过程，完全气体假设将不再适用。两种效应强烈耦合形成高温湍流，进而带来高温边界层扰动演化与多尺度涡结构、高温强扰动下气固界面多相反应、极端高温环境等离子体湍流等新的流动物理问题。本文从机理、预测、实验测量等方面，总结了高速高温湍流领域的研究进展和现状，展望了未来需要关注的研究方向。

Abstract

Future advanced air vehicles demonstrate a development trend towards high-speed flight in low-altitude airspace so that boundary layers over the aircraft high Mach numbers

high Reynolds numbers

and high total enthalpy feature. Higher Reynolds numbers lead to the boundary layer transition from laminar to turbulent states. The high-temperature environment

induced by the compression of intense shock waves

results in a thermochemical non-equilibrium state encompassing the effects of vibration excitation

dissociation

and ionization that invalidate the perfect gas assumption. The deeply intertwined high-temperature and high-Reynolds-number effects give rise to the high-temperature turbulence

which introduces novel flow physics including the disturbances evolution and multiscale flow structures in high-enthalpy boundary layers

gas-solid multiphase reactions under high-temperature and strong disturbances

as well as plasma turbulence in extremely high-temperature environments. This study provides a comprehensive overview of the research progress and current status regarding high-temperature turbulence mechanisms

prediction

and experimental measurements. Furthermore

it outlines the future research directions that deserve attention.

关键词

Keywords

references

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