空气动力学学报2024，Vol.42Issue(4)：1-13,13.DOI:10.7638/kqdlxxb-2023.0185
高速高温湍流研究进展
Progress in high-speed high-temperature turbulence research
摘要
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
高马赫数/湍流/高温非平衡/表面效应/电磁效应Key words
high Mach number/turbulence/high-temperature non-equilibrium/surface effects/electromagnetic effect分类
航空航天引用本文复制引用
袁先旭,刘朋欣,周清清,傅亚陆,杨肖峰,杜雁霞..高速高温湍流研究进展[J].空气动力学学报,2024,42(4):1-13,13.基金项目
国家重点研发计划(2019YFA0405200) （2019YFA0405200）
国家自然科学基金(12272396) （12272396）
