高速飞行器减阻降热流动控制技术研究进展及工程应用
收稿日期: 2023-05-23
修回日期: 2023-05-26
录用日期: 2023-06-06
网络出版日期: 2023-06-06
基金资助
国家自然科学基金(U21B6003)
Research progress and engineering application of flow control technology for drag and heat reduction of high-speed vehicles
Received date: 2023-05-23
Revised date: 2023-05-26
Accepted date: 2023-06-06
Online published: 2023-06-06
Supported by
National Natural Science Foundation of China(U21B6003)
朱广生 , 姚世勇 , 段毅 . 高速飞行器减阻降热流动控制技术研究进展及工程应用[J]. 航空学报, 2023 , 44(15) : 529049 -529049 . DOI: 10.7527/S1000-6893.2023.29049
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.
Key words： flow control; drag reduction; heat reduction; shock wave; boundary layer
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