The primary focus of the present survey is to categorize the results of various investigations on the Shock/Boundary-Layer Interactions (SBLIs), their repercussions, and the effective ways to control them. The interactions of shock waves with the boundary layer are an important area of research due to their ubiquity in several applications ranging from transonic to hypersonic flows. Therefore, there is a need for a detailed inspection to understand the phenomena to predict its characteristics with certain accuracy. Considering this in mind, this article presents some key features of the physical nature of SBLIs, their consequences, and the control techniques in a sequential manner; in particular, the passive control techniques for the supersonic and hypersonic intakes are reviewed in detail. 1. Shock/Boundary-Layer Interactions (SBLIs) and their consequences in high-speed aircraft are reviewed. 2. Various active and passive control strategies that have been used to mitigate the effects of SBLI are addressed. 3. The efficacy of Porous Cavity and Micro-Vortex Generators in controlling SBLI is described in detail.

中文翻译：

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减轻冲击波和边界层相互作用影响的控制技术调查

本次调查的主要重点是对冲击/边界层相互作用 (SBLI) 的各种调查结果、它们的影响以及控制它们的有效方法进行分类。冲击波与边界层的相互作用是一个重要的研究领域，因为它们在从跨音速到高超音速流的多种应用中无处不在。因此，需要进行详细的检查以了解现象，从而以一定的准确性预测其特征。考虑到这一点，本文按顺序介绍了 SBLI 的物理性质、其后果和控制技术的一些关键特征；特别是对超音速和高超音速进气道的被动控制技术进行了详细回顾。1. 冲击/边界层相互作用（SBLIs）及其在高速飞机中的后果进行了审查。2. 解决了已用于减轻 SBLI 影响的各种主动和被动控制策略。3. 详细描述了多孔腔和微涡流发生器在控制 SBLI 中的功效。