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Titlebook: New Results in Numerical and Experimental Fluid Mechanics IX; Contributions to the Andreas Dillmann,Gerd Heller,Ulrich Rist Book 2014 Sprin

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書目名稱New Results in Numerical and Experimental Fluid Mechanics IX
副標(biāo)題Contributions to the
編輯Andreas Dillmann,Gerd Heller,Ulrich Rist
視頻videohttp://file.papertrans.cn/666/665728/665728.mp4
概述Latest research in numerical and experimental fluid mechanics and aerodynamics for (but not limited to) aerospace applications.Collection of contributions presented during the 18th Symposium of the ST
叢書名稱Notes on Numerical Fluid Mechanics and Multidisciplinary Design
圖書封面Titlebook: New Results in Numerical and Experimental Fluid Mechanics IX; Contributions to the Andreas Dillmann,Gerd Heller,Ulrich Rist Book 2014 Sprin
描述.This book presents contributions to the 18th biannual symposium of the German Aerospace Aerodynamics Association (STAB). 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. By addressing a number of essential research subjects, together with their related physical and mathematics fundamentals, the book provides readers with a comprehensive overview of the current research work in the field, as well as its main challenges and new directions. Current work on e.g. high aspect-ratio and low aspect-ratio wings, bluff bodies, laminar flow control and transition, active flow control, hypersonic flows, aeroelasticity, aeroacoustics and biofluid mechanics is exhaustively discussed here..
出版日期Book 2014
關(guān)鍵詞18th STAB/DGLR Symposium; Airplane Aerodynamics; Biofluid Mechanics; Blade-design; Convective Flows; DNS
版次1
doihttps://doi.org/10.1007/978-3-319-03158-3
isbn_softcover978-3-319-35322-7
isbn_ebook978-3-319-03158-3Series ISSN 1612-2909 Series E-ISSN 1860-0824
issn_series 1612-2909
copyrightSpringer International Publishing Switzerland 2014
The information of publication is updating

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The Influence of the Diffusion Model on the Separation Sensitivity of Differential Reynolds Stress Mc aerodynamic test cases. While there is very little influence on the pressure distribution, some differences are observed in the predicted skin friction, revealing the more complex diffusion models to enhance the sensitivity to separation.
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Numerical Approach Aspects for the Investigation of the Longitudinal Static Stability of a TransportThe aim of the investigation is to gain more certainty about the approach to evaluate the longitudinal stability and controllability of a high-lift configuration of a transport aircraft with circulation control. Since the work was carried out with a CFD RANS approach, a comprehensive meshing study was performed in advance.
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978-3-319-35322-7Springer International Publishing Switzerland 2014
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Efficient Global Optimization of a Natural Laminar Airfoil Based on Surrogate Modelingn with the adaptive sample refinement strategies features a good balance between global exploration and local exploitation. Additionally, the effect of different design points on the objective function can be automatically considered in the refinement procedure.
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