【摘要】 针对高超声速进气道V形溢流口处极易形成复杂激波干扰，并产生严酷气动热/力载荷的问题，本文梳理和总结了近年来提炼模化出的V形钝化前缘（VBLE）及其相关研究的进展情况。回顾了V形钝化前缘模型的提出过程，介绍了其几何及流动的主要特点，分析了V形钝化前缘的激波干扰类型、气动热/力载荷以及激波振荡特性，探讨了降低局部极高气动热/力载荷及抑制激波振荡的优化设计方案，并对未来的研究方向进行了展望，以期促进对V形钝化前缘激波干扰现象的深入理解。更多还原

【Abstract】 A V-shaped cowl lip is commonly designed for flow spillage in hypersonic inward-turning inlets, which leads to complex flow structures and severe aerothermal/pressure load. A number of investigations has been performed to understand the shock interactions and underlying mechanisms, since a generic V-shaped Blunt Leading Edge(VBLE) was proposed. The types of the shock interactions, characteristics of aerothermal/pressure load, unsteady shock oscillations,and aerodynamic optimization of the VBLE were reviewed, after a retrospection of the naissance of the VBLE. Finally, future work was discussed to improve knowledge of the VBLE to a new horizon.更多还原