实验流体力学2017，Vol.31Issue(2)：1-11,11.DOI:10.11729/syltlx20160129
高超声速边界层感受性研究综述
Review of research on the receptivity of hypersonic boundary layer
摘要
Abstract
As a key aspect of transition prediction and control, receptivity process in hypersonic boundary layer is of great importance.However, it still has not been thoroughly understood, and is especially lacking in experimental verification.In this paper, two categories of disturbances are reviewed, namely, free-stream disturbance (acoustic, vertical, thermal perturbation, shock wave and particulates) and wall-induced disturbances (roughness, vibration, blowing and suction, surface heating and cooling).Mostly concerned are the theory of Fedorov about leading-edge receptivity and inter-modal exchange mechanism.In order to make the issue of receptivity more clearly understood, a compendious path diagram is sketched to describe paths to Mack modes.关键词
高超声速边界层/感受性/综述/理论研究/声波/粗糙元/壁面温度Key words
hypersonic boundary layer/receptivity/review/theory research/acoustic/roughness/wall temperature分类
数理科学引用本文复制引用
江贤洋,李存标..高超声速边界层感受性研究综述[J].实验流体力学,2017,31(2):1-11,11.基金项目
国家自然科学基金资助项目"高超声速边界层控制转捩研究"(11632002) （11632002）
"可压缩湍流的机理、模式及实验研究"(11521091) （11521091）
"壁面温度对高超声速边界层转捩影响的实验研究"(11602005) （11602005）
