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Titlebook: Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines and Propellers; H. M. Atassi (Symposium Chairman) Conference pro

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书目名称Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines and Propellers
编辑H. M. Atassi (Symposium Chairman)
视频video
图书封面Titlebook: Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines and Propellers;  H. M. Atassi (Symposium Chairman) Conference pro
描述The first International Symposium on Unsteady Aerodynamics and Aero­ elasticity of Turbomachines was held in Paris in 1976, and was followed by symposia at Lausanne in 1980, Cambridge in 1984, Aachen in 1987, Bei­ jing in 1989, and Notre Dame in 1991. The proceedings published following these symposia have become recognized both as basic reference texts in the subject area and as useful guides to progress in the field. It is hoped that this volume, which represents the proceedings of the Sixth International Symposium on Unsteady Aerodynamics of Turbomachines, will continue that tradition. Interest in the unsteady aerodynamics, aeroacoustics, and aeroelasticity of turbomachines has been growing rapidly since the Paris symposium. This expanded interest is reflected by a significant increase in the numbers of contributed papers and symposium participants. The timeliness of the topics has always been an essential objective of these symposia. Another important objective is to promote an international exchange between scien­ tists and engineers from universities, government agencies, and industry on the fascinating phenomena of unsteady turbomachine flows and how they affect the aeroelas
出版日期Conference proceedings 1993
关键词Vibration; acoustics; aerodynamics; dynamics; elasticity
版次1
doihttps://doi.org/10.1007/978-1-4613-9341-2
isbn_softcover978-1-4613-9343-6
isbn_ebook978-1-4613-9341-2
copyrightSpringer-Verlag New York, Inc. 1993
The information of publication is updating

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书目名称Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines and Propellers网络公开度学科排名




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Unsteady Aerodynamic Methodsor the effects of realistic design features, such as real blade geometry, mean blade loading and operation at transonic Mach numbers, on the unsteady aerodynamic response of two-dimensional cascades. The improvements in physical modeling that such linearizations allow are motivating their current im
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Long Time Behavior of Unsteady Flow Computationshis applies to the convective wave equation as well. The consequences are rather severe if one focuses on the time accuracy of solutions of problems governed by the Euler equations..In concert with the above mentioned problem, exterior flows require proper modeling of boundary conditions. Computatio
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Time Linearized Euler Calculations for Unsteady Quasi-3D Cascade Flowsl for both solvers. Thus it is possible to use much of the steady code with little modification for the time-linearized unsteady code..Because of the linearity of the unsteady equations, they can be solved very efficiently by an ADI-method..The results obtained by this method compare favourably to f
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Unsteady Flow Field Predictions for Oscillating Cascadesng uniform grids as long as the CFL number is less than one for a sufficient portion of the grid. Finally, a solution based on an optimization of grid, CFL number and boundary conditions shows good agreement with linear theory.
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