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Article

Hypersonic Leading-Edge Cooling—A Comprehensive Review

School of Mechanical, Aerospace, and Materials Engineering, College of Engineering, Computing, Technology, and Mathematics, Southern Illinois University, Carbondale, IL 62901, USA
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Aerospace 2026, 13(7), 573; https://doi.org/10.3390/aerospace13070573 (registering DOI)
Submission received: 15 December 2025 / Revised: 12 June 2026 / Accepted: 12 June 2026 / Published: 25 June 2026
(This article belongs to the Special Issue High Speed Aircraft and Engine Design)

Abstract

Human innovation has continually expanded the boundaries of knowledge, from mastering atomic science to reaching the Moon and now into the era of Industry 4.0, where artificial intelligence, the Internet, and advanced additive manufacturing turn imagination into reality. Among these achievements, hypersonic vehicles represent a pinnacle of technological advancement. Modern vehicles reach speeds exceeding Mach 27 (approximately 9300 m/s), where the air at the leading edges transforms into a chemically reactive, thermally ionized plasma. At such velocities, stagnation temperatures climb to 9000–12,000 K (8726.85–11,726.85 °C), creating one of the most extreme environments encountered by any human-made system—conditions under which conventional materials cannot survive without advanced cooling strategies. To address this challenge, researchers worldwide have developed and experimentally validated a range of thermal protection and leading-edge cooling techniques. This review presents the historical evolution of hypersonic vehicles, highlights recent advancements, examines the key challenges posed by sustained hypersonic flight, and surveys state-of-the-art cooling strategies. The discussion emphasizes methods that combine passive, active, adaptive, and hybrid approaches to protect vehicle integrity under extreme thermal loads, providing insight into the current and future capabilities of hypersonic thermal manageme nt.
Keywords: hypersonic vehicles; leading-edge cooling; thermal protection systems (TPS); transpiration cooling; aerothermal heating hypersonic vehicles; leading-edge cooling; thermal protection systems (TPS); transpiration cooling; aerothermal heating

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MDPI and ACS Style

Aleemuddin, M.; Hossain, M.A.; Barua, A. Hypersonic Leading-Edge Cooling—A Comprehensive Review. Aerospace 2026, 13, 573. https://doi.org/10.3390/aerospace13070573

AMA Style

Aleemuddin M, Hossain MA, Barua A. Hypersonic Leading-Edge Cooling—A Comprehensive Review. Aerospace. 2026; 13(7):573. https://doi.org/10.3390/aerospace13070573

Chicago/Turabian Style

Aleemuddin, Mohammed, Md Amzad Hossain, and Adittya Barua. 2026. "Hypersonic Leading-Edge Cooling—A Comprehensive Review" Aerospace 13, no. 7: 573. https://doi.org/10.3390/aerospace13070573

APA Style

Aleemuddin, M., Hossain, M. A., & Barua, A. (2026). Hypersonic Leading-Edge Cooling—A Comprehensive Review. Aerospace, 13(7), 573. https://doi.org/10.3390/aerospace13070573

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