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Titlebook: Numerical and Physical Aspects of Aerodynamic Flows; Tuncer Cebeci Conference proceedings 1982 Springer Science+Business Media New York 19

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書(shū)目名稱(chēng)Numerical and Physical Aspects of Aerodynamic Flows
編輯Tuncer Cebeci
視頻videohttp://file.papertrans.cn/670/669255/669255.mp4
圖書(shū)封面Titlebook: Numerical and Physical Aspects of Aerodynamic Flows;  Tuncer Cebeci Conference proceedings 1982 Springer Science+Business Media New York 19
描述This volume contains revised and edited forms of papers presented at the Symposium on Numerical and Physical Aspects of Aerodynamic Flows, held at the California State University from 19 to 21 January 1981. The Symposium was organized to bring together leading research workers in those aspects of aerodynamic flows represented by the five parts and to fulfill the following purposes : first, to allow the presentation of technical papers which provide a basis for research workers to assess the present status of the subject and to formulate priorities for the future; and second, to promote informal discussion and thereby to assist the communication and develop- ment of novel concepts. The format ofthe content ofthe volume is similar to that ofthe Symposium and addresses, in separate parts: Numerical Fluid Dynamics, Interactive Steady Boundary Layers, Singularities in Unsteady Boundary Layers, Transonic Flows, and Experimental Fluid Dynamics. The motivation for most of the work described relates to the internal and extern al aerodynamics of aircraft and to the development and appraisal of design methods based on numerical solutions to conservation equations in differential forms, for co
出版日期Conference proceedings 1982
關(guān)鍵詞Flows; Grenzschicht; Numerische Mathematik; Schallnahe Str?mung; Str?mung; fluid dynamics; fluid- and aero
版次1
doihttps://doi.org/10.1007/978-3-662-12610-3
isbn_softcover978-3-662-12612-7
isbn_ebook978-3-662-12610-3
copyrightSpringer Science+Business Media New York 1982
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Experiments on Initial and Boundary Conditionsntal interferences. Data obtained by the Wright brothers in their historic wind tunnel enabled them to evaluate the possibility of flying; by current standards they would probably not even fit in what engineers call the “ballpark” range. The designer’s problem is efficiency; errors larger than 1% in
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Some Observations on Numerical Solutions of the Three-Dimensional Navier-Stokes Equationsions. These flows may be either laminar or turbulent or both, and for laminar flow the use of the three-dimensional Navier-Stokes equations is required to adequately represent the motion. For turbulent flows, these same equations are usually ensemble-averaged, and with the introduction of current-ge
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Some Recent Studies in Triple-Deck Theorya continual challenge to theoreticians for many years. The usual approach, and one which I favor, is to regard it as controlled by an interaction between an external inviscid and a viscous boundary layer. For some time the discovery [2.8] that a laminar boundary layer invariably appears to become si
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