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Titlebook: Symposium Transsonicum III; IUTAM Symposium Gött J. Zierep,H. Oertel Conference proceedings 1989 Springer-Verlag Berlin Heidelberg 1989 CFD

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书目名称Symposium Transsonicum III
副标题IUTAM Symposium Gött
编辑J. Zierep,H. Oertel
视频video
丛书名称IUTAM Symposia
图书封面Titlebook: Symposium Transsonicum III; IUTAM Symposium Gött J. Zierep,H. Oertel Conference proceedings 1989 Springer-Verlag Berlin Heidelberg 1989 CFD
描述Continuing the tradition of the IUTAM Symposia TRANSSONICA, this review of the numerical simulation and physical modelling of transonic flows presents new developments in the fields of computational and experimental aerodynamics. A major topic of the symposium proceedings is the evaluation of present numerical analysis techniques with respect to transonic aerodynamics. In the field of experimental aerodynamics, the high Reynolds number effect and the interference-free testing in transonic wind tunnels are of special interest.
出版日期Conference proceedings 1989
关键词CFD; Natur; Software; aerodynamics; aircraft design; design; development; dynamics; simulation
版次1
doihttps://doi.org/10.1007/978-3-642-83584-1
isbn_softcover978-3-642-83586-5
isbn_ebook978-3-642-83584-1
copyrightSpringer-Verlag Berlin Heidelberg 1989
The information of publication is updating

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Zonal Solutions of Three-Dimensional Viscous Flow Problemsupled Euler/boundary-layer equations are employed. CCPNS is an option in the governing Navier-Stokes code NSFLEX to reduce computation cost. Several applications demonstrate the efficiency of the method. Good agreement with full NSFLEX results is achieved.
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On the Computation of Transonic Viscous Flowshe numerical results by comparison with the experiment renders more difficult, since now uncertainties of both are superposed. In particular cases correlations between numerical and experimental results could be achieved only by “trial and error”.
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Some Asymptotic Problems of Transonic Flow Theoryess ratio . = . (.). The matching of these expansions defines suitable boundary value problems. Second, expansions in terms of the similarity parameter . show the generalization of the Law of Stabilization for this case.
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Conference proceedings 1989t numerical analysis techniques with respect to transonic aerodynamics. In the field of experimental aerodynamics, the high Reynolds number effect and the interference-free testing in transonic wind tunnels are of special interest.
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Summary and Evaluation of the Workshop “Numerical Simulation of Compressible Viscous-Flow Aerodynami code validation purposes. Thus, the experimental data allow to formulate analytically the corresponding boundary value problem for the integration of the Navier-Stokes equations. Based on the experiment a workshop took place. Results of the numerical simulations are compared with each other and wit
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