舰载航空飞行器气动技术发展趋势研究  

Research on the development trend of aerodynamic technology for the carrier-based aerial vehicle

作　　者：刘晓波[1] 陈涛 孙杭义 钟萍[1] 何思利 石建军[2] 周蜜 Liu Xiaobo;Chen Tao;Sun Hangyi;Zhong Ping;He Sili;Shi Jianjun;Zhou Mi(Computational Aerodynamics Institute,China Aerodynamics Research and Development Center,Mianyang 621000,China;School of Civil Engineering and Architecture,Department of Engineering Mechanics,Southwest University of Science and Technology,Mianyang 621010,China)

机构地区：[1]中国空气动力研究与发展中心计算空气动力研究所,绵阳621000 [2]西南科技大学土木工程与建筑学院工程力学系,绵阳621010

出　　处：《战术导弹技术》2024年第5期30-39,共10页Tactical Missile Technology

摘　　要：针对舰载航空飞行器的应用背景和发展现状,综述了舰载航空飞行器的主要类型及其存在的特殊空气动力学问题,研究了美国在解决舰载航空飞行器空气动力学问题方面的方法,阐述了利用数值仿真、地面试验、飞行试验三种研究手段所开展的具体研究工作和获得的研究成果,展望了舰载航空飞行器气动技术的未来发展趋势,主要包括在气动布局技术上将重点发展高升力构型和无尾飞翼构型,在流动控制技术上将综合考虑主动流动控制技术与被动流动控制技术的结合,在地面试验技术上将结合无人机的试验需求发展多空间维度的试验技术,在飞行控制技术上将根据悬停能力、高速飞行、自主着舰、编队飞行等任务需求发展多项新型飞行控制技术。Focusing on the application background and development status of the carrier-based aerial vehicle,a brief introduction of its types and special aerodynamic issues presented.The way the United States overcomes aerodynamic problem is studied,especially for its research work and excellent achievements through three classical methods including numerical simulation,ground test and flight test.The development trend of aerodynamic technology involved in carrier-based aerial vehicle is prospected from the perspectives of aerodynamic configuration technology that highlights on high-lift configuration and tailless fly-wing configuration,flow control technology that combines active and passive flow control,ground test technology that develops multiple-space dimension test meeting the needs of unmanned aircraft,and flight control technology that underscores the development of several novel flight control technology in terms of hover and advancing flight ability,autonomous landing and teamed flight.

关 键 词：舰载航空飞行器 空气动力技术 数值仿真 地面试验 飞行试验 气动布局 流动控制 

分 类 号：V411[航空宇航科学与技术—航空宇航推进理论与工程]