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Shock wave rod based on supercritical fluid coolant, heat protection device and method
High-speed nose cone combined cooling structure and method based on supercritical fluid
Design and Performance of a Hypersonic Quiet Wind Tunnel at NUDT (AIAA 2017-2305)
High-speed boundary layer transition control device and control method based on micro-nano gas film
Underwater vehicle drag reduction device based on permeable gas film
Airfoil with leading edge cooling structure and high-speed aircraft