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This document is a summary of a special issue of the journal Aerospace titled "Shock-Dominated Flow." The issue, guest-edited by Dr. He-xia Huang, Professor Hui-jun Tan, and Professor Ye Tian, consists of 10 articles that focus on the fluid mechanics and flow control methods of shock-dominated flows. The articles provide new insights into this research field, which is important for high-speed aircraft, engines, and missiles. The issue covers topics such as hypersonic inlets, shock-induced separation, dynamic mode decomposition, and various flow control methods. These methods include vortex generators, micro-serrations, plasma-based flow control, and dielectric barrier discharge plasma actuators. The issue also includes a study on shock diffraction in muzzle jets. The summary concludes by acknowledging the authors, reviewers, and editorial office for their contributions to the special issue. [Extracted from the article]