Research progress and engineering application of flow control technology for drag and heat reduction of high-speed vehicles

被引：0
作者：
Zhu G. [1 ]
Yao S. [1 ,2 ]
Duan Y. [1 ,2 ]
机构：
[1] China Academy of Launch Vehicle Technology, Beijing
[2] Science and Technology on Space Physics Laboratory, China Academy of Launch Vehicle Technology, Beijing
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2023年 / 44卷 / 15期
基金：
中国国家自然科学基金;
关键词：
boundary layer; drag reduction; flow control; heat reduction; shock wave;
D O I：
10.7527/S1000-6893.2023.29049
中图分类号：
学科分类号：
摘要：
Drag and heat reductions are two core issues in the design of high-speed flight vehicles. Drag reduction can enhance the lift-drag ratio of vehicles and decrease the fuel consumption，while heat reduction can reduce the weight of thermal protection system and promote the effective load of flight vehicles. Drag and heat reductions are the key technologies to improve the fine design and enhance the flight performance. This paper mainly reviews the research status of flow control technology for drag and heat reductions of shock wave and boundary layer，from the perspective of the engineering requirements for drag and heat reductions of high-speed flight vehicles. This paper also points out the existing problems in engineering application and the direction that should be paid close attention to in the future，to realize the engineering application of active flow control of flight vehicles and improve the flight performance. © 2023 AAAS Press of Chinese Society of Aeronautics and Astronautics. All rights reserved.
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