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Titlebook: New Results in Numerical and Experimental Fluid Mechanics XII; Contributions to the Andreas Dillmann,Gerd Heller,Suad Jakirlić Conference p

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书目名称New Results in Numerical and Experimental Fluid Mechanics XII
副标题Contributions to the
编辑Andreas Dillmann,Gerd Heller,Suad Jakirlić
视频video
概述Reports on numerical simulation and experimental results in fluid mechanics.Includes contributions to the 21st symposium (2018) of the German Aerospace Aerodynamics Association (STAB).Describes the la
丛书名称Notes on Numerical Fluid Mechanics and Multidisciplinary Design
图书封面Titlebook: New Results in Numerical and Experimental Fluid Mechanics XII; Contributions to the Andreas Dillmann,Gerd Heller,Suad Jakirlić Conference p
描述.This book gathers contributions to the 21.st. biannual symposium of the German Aerospace Aerodynamics Association (STAB) and the German Society for Aeronautics and Astronautics (DGLR). The individual chapters reflect ongoing research conducted by the STAB members in the field of numerical and experimental fluid mechanics and aerodynamics, mainly for (but not limited to) aerospace applications, and cover both nationally and EC-funded projects. Special emphasis is given to collaborative research projects conducted by German scientists and engineers from universities, research-establishments and industries. By addressing a number of cutting-edge applications, together with the relevant physical and mathematics fundamentals, the book provides readers with a comprehensive overview of the current research work in the field. The book’s primary emphasis is on aerodynamic research in aeronautics and astronautics, and in ground transportation and energy as well..
出版日期Conference proceedings 2020
关键词Boundary Layer Transition; Turbulent Flow Separation; Laminar Flow Control; Optimization of Wings; Aerod
版次1
doihttps://doi.org/10.1007/978-3-030-25253-3
isbn_softcover978-3-030-25255-7
isbn_ebook978-3-030-25253-3Series ISSN 1612-2909 Series E-ISSN 1860-0824
issn_series 1612-2909
copyrightSpringer Nature Switzerland AG 2020
The information of publication is updating

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Unsteady Wake and Tailplane Loads of the Common Research Model in Low Speed Stallthe interaction of the separated wake with the tailplane in the presence of massively separated flow on the main wing. Validation of the CFD data using PIV data obtained for the flow conditions at ., . and . was carried out, confirming the generally satisfactory performance of the DDES simulations o
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Modification of the SSG/LRR-, RSM for Turbulent Boundary Layers at Adverse Pressure Gradient with Sewhich was performed within the DLR project VicToria. We describe the design of the test case, the set-up in the wind-tunnel, and the measurement technique using particle imaging and particle tracking with the novel Shake-The-Box technique. We present the experimental results for the mean velocity pr
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