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Titlebook: Numerical and Physical Aspects of Aerodynamic Flows II; Tuncer Cebeci Conference proceedings 1984 Springer Science+Business Media New York

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書目名稱Numerical and Physical Aspects of Aerodynamic Flows II
編輯Tuncer Cebeci
視頻videohttp://file.papertrans.cn/670/669256/669256.mp4
圖書封面Titlebook: Numerical and Physical Aspects of Aerodynamic Flows II;  Tuncer Cebeci Conference proceedings 1984 Springer Science+Business Media New York
描述The Second Symposium on Numerical and Physical Aspects of Aerodynamic Flows was held at California State University, Long Beach, from 17 to 20 January 1983. Forty-eight papers were presented, including Keynote Lec- tures by A. M. 0. Smith and J. N. Nielsen, in ten technical sessions which were supplemented and complemented by two Open Forum Sessions, involving a further sixteen technical presentations and a Panel Discussion on the "Identification of priorities for the development of calculation methods for aerodynamic bodies. " The Symposium was attended by 120 research workers from nine countries and, as in the First Symposium, provided a basis for research workers to communicate, to assess the present status of the subject and to formulate priorities for the future. In contrast to the First Symposium, the papers and discussion were focused more clearly on the subject of flows involving the interaction between viscous and inviscid regions and the calculation of pressure, velocity and temperature characteristics as a function of geometry, angle of attack and Mach number. Rather more than half the papers were concerned with two-dimensional configurations and the remainder with wings
出版日期Conference proceedings 1984
關(guān)鍵詞Flows; Grenzschicht; Str?mung; Tragflügel; development; entropy; geometry; information; laminar flow; paper; s
版次1
doihttps://doi.org/10.1007/978-3-662-09014-5
isbn_softcover978-3-662-09016-9
isbn_ebook978-3-662-09014-5
copyrightSpringer Science+Business Media New York 1984
The information of publication is updating

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Global Solution Procedures for Incompressible Laminar Flow with Strong Pressure Interaction and Sepaer and triple deck formulations, an alternate development that more closely follows these asymptotic theories is considered here for the evaluation of laminar interacting flows at large Reynolds numbers.
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Calculation of Two-Dimensional Flow Past Airfoilsct representation of transition and turbulent flow processes. At transonic speeds the appearance of shocks in the inviscid part of the flow field and their interaction with the boundary layer represent additional difficulties.
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Conference proceedings 1984 1983. Forty-eight papers were presented, including Keynote Lec- tures by A. M. 0. Smith and J. N. Nielsen, in ten technical sessions which were supplemented and complemented by two Open Forum Sessions, involving a further sixteen technical presentations and a Panel Discussion on the "Identification
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