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Titlebook: Laminar-Turbulent Transition; IUTAM Symposium, Sed Hermann F. Fasel,William S. Saric Conference proceedings 2000 Springer-Verlag Berlin Hei

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发表于 2025-3-21 19:17:35 | 显示全部楼层 |阅读模式
书目名称Laminar-Turbulent Transition
副标题IUTAM Symposium, Sed
编辑Hermann F. Fasel,William S. Saric
视频videohttp://file.papertrans.cn/581/580522/580522.mp4
概述Includes supplementary material:
丛书名称IUTAM Symposia
图书封面Titlebook: Laminar-Turbulent Transition; IUTAM Symposium, Sed Hermann F. Fasel,William S. Saric Conference proceedings 2000 Springer-Verlag Berlin Hei
描述The origins of turbulent flow and the transition from laminar to turbulent flow are among the most important unsolved problems of fluid mechanics and aerodynamics. Besides being a fundamental question of fluid mechanics, there are any number of applications for information regarding transition location and the details of the subsequent turbulent flow. The JUT AM Symposium on Laminar-Turbulent Transition, co-hosted by Arizona State University and the University of Arizona, was held in Sedona, Arizona. Although four previous JUT AM Symposia bear the same appellation (Stuttgart 1979, Novosibirsk 1984, Toulouse 1989, and Sendai 1994) the topics that were emphasized at each were different and reflect the evolving nature of our understanding of the transition process. The major contributions of Stuttgart 1979 centered on nonlinear behavior and later stages of transition in two-dimensional boundary layers. Stability of closed systems was also included with Taylor vortices in different geometries. The topics of Novosibirsk 1984 shifted to resonant wave interactions and secondary instabilities in boundary layers. Pipe- and channel-flow transition were discussed as model problems for the bou
出版日期Conference proceedings 2000
关键词Aerodynamics; Aerodynamik; Fluid mechanics; Hydrodynamics; Hydrodynamik; Turbulence; Turbulenz; mechanics; f
版次1
doihttps://doi.org/10.1007/978-3-662-03997-7
isbn_softcover978-3-642-08752-3
isbn_ebook978-3-662-03997-7
copyrightSpringer-Verlag Berlin Heidelberg 2000
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Effect of Leading-edge Geometry and Aerodynamic Loading on Receptivity to Acoustic Disturbancesar, time-harmonic disturbances to a two-dimensional, low Mach number flow past a cambered airfoil with parabolic leading edge. Asymptotic methods based on large Reynolds number are used, supplemented by numerical results. The body nose radius enters the theory through a Strouhal number ., and the me
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Three-Dimensional Receptivity of Boundary Layers to External Perturbationsnd has both basic and practical significance. In the present paper a very brief review of studies (mainly the experimental ones) performed during past several years is carried out. The generation of two kinds of the instability modes is discussed: (.) the Tollmien-Schlichting (TS) waves and (.) the
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Non-localized acoustic receptivity and subsequent disturbance growth in a Blasius boundary layer Linear receptivity coefficients obtained for all values of forcing combinations (. · .) are in good agreement with receptivity theory. The measured receptivity increased markedly with increasing wave obliqueness. Detuning was investigated by varying the streamwise wavenumber, .., of the 2-D and obl
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Receptivity and Bypass Dynamics problem with an inhomogeneous forcing term imposed upon the flow are sought. It is shown that: (1) A transient disturbance lying located outside of the boundary layer can lead to the growth of an unstable Tollmein-Schlicting wave; (2) A resonance with the continuous spectrum may provide a mechanism
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