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定常升阻力:基础理论的主流演化 被引量:3

Steady Lift and Drag:The Mainstream Evolution of Fundamental Theory
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摘要 本文专注于飞行器定常绕流升阻力的关键物理机理和精确理论。自古以来,人类对飞得更高、更快、更远的梦想和追求从未停止。从20世纪初莱特兄弟实现载人动力飞行和Kutta-Joukowski升力公式问世开始,空气动力学理论经历了一个多世纪的曲折探索,从无黏到有黏、从定常到非定常、从不可压到可压缩、从近似到精确,已经发展出众多关于升力和阻力的理论,在实践中得到了多方面的充分检验,为航空航天、流体机械、风工程等众多应用领域提供了不可或缺的基础保证。 This paper focuses on the key physical mechanisms and rigorous theories of aircraft lift and drag in steady flow.Since ancient times,human beings have never stopped dreaming and pursuing to fly higher,faster and farther.Since the Wright brothers realized manned power flight and the Kutta-Joukowski lift formula came out in the early 20th century,aerodynamics has gone through more than a century of tortuous exploration,from inviscid to viscous,from steady to unsteady,from incompressible to compressible,from approximate to precise,leading to a series of lift and drag theories.It has been fully tested in various practical aspects and provides an indispensable basic guarantee for many applied fields such as aerospace,fluid machinery,and wind engineering.
作者 刘罗勤 邹舒帆 朱金阳 康林林 高安康 吴介之 Liu Luoqin;Zou Shufan;Zhu Jinyang;Kang Linlin;Gao Ankang;Wu Jiezhi(School of Engineering Science,University of Science and Technology of China,Hefei 230027,China;College of Aerospace Science and Engineering,National University of Defense Technology,Changsha 410000,China;China Electric Power Planning&Engineering Institute,Beijing 100120,China;School of Engineering,Westlake University,Hangzhou 310024,China;College of Engineering,Peking University,Beijing 100871,China)
出处 《气动研究与试验》 2023年第5期1-35,共35页 Aerodynamic Research & Experiment
关键词 Kutta-Joukowski升力公式 Filon阻力公式 Prandtl涡力理论 黏性升阻力理论 可压缩涡力理论 诱导阻力 型阻 波阻 Mach数相似律 定常升阻力的普适远场理论 Kutta-Joukowski lift formula Filon drag formula Prandtl vortex-force theory viscous lift-drag theory compressible vortex-force theory induced drag profile drag wave drag Mach number similarity laws universal far-field theory of steady lift and drag
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