高速飞行器减阻降热研究进展  

Current status of research on reducing drag and cooling of high-speed aircraft

作　　者：潘利生[1,2] 郝亨隆 姚子康 郭媛 慕浩凡 李敏 魏小林 PAN Lisheng;HAO Henglong;YAO Zikang;GUO Yuan;MU Haofan;LI Min;WEI Xiaolin(State Key Laboratory of High-temperature Gas Dynamics,Institute of Mechanics,Chinese Academy of Sciences,Beijing 100190,China;School of Environment and Energy Engineering,Beijing University of Civil Engineering and Architecture,Beijing 100049,China;School of Engineering Science,University of Chinese Academy of Science,Beijing 100044,China)

机构地区：[1]中国科学院力学研究所高温气体动力学国家重点实验室,北京100190 [2]中国科学院大学工程科学学院,北京100049 [3]北京建筑大学环境与能源工程学院,北京100044

出　　处：《力学进展》2023年第4期793-818,共26页Advances in Mechanics

摘　　要：降低飞行阻力、探索更高效的热防护系统是研发高速飞行器过程中至关重要的课题.目前,国内外学者在飞行器减阻降热的机理及应用技术方面进行了大量研究,取得了丰富的成果.本文系统地梳理了在高速飞行器减阻降热领域的研究进展,阐述了主动热防护机理的研究结果,介绍了应用于高速飞行器的前沿减阻降热技术,并简述了基于余热利用的整体热防护系统的发展情况.基于对研究现状的分析,归纳总结了高速飞行器减阻降热技术的发展趋势与实际研究需求;最后针对这些实际研究需求,提出了一些研究思路上的建议.Reducing flight resistance and exploring more efficient thermal protection systems are crucial issues in the development of high-speed aircraft.Domestic and foreign scholars have conducted extensive research on the mechanism and application technology of aircraft cooling and drag reduction,and have achieved rich results.This article systematically reviews the research progress in the field of cooling and drag reduction for hypersonic aircraft,elaborates on the research results of active thermal protection mechanisms,introduces cooling and drag reduction technologies applied to high-speed aircraft,And briefly described the development of overall thermal protection systems based on waste heat utilization.Based on the analysis of the current research status,the development trend and practical research needs of drag and heat reduction technology for high-speed aircraft were summarized and summarized.Finally,in response to these practical research needs,some suggestions on research ideas were proposed.

关 键 词：飞行器主动冷却技术 主动流动控制 减阻降热 综合热管理系统 

分 类 号：V37[航空宇航科学与技术—航空宇航推进理论与工程]