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Titlebook: New Results in Numerical and Experimental Fluid Mechanics VII; Contributions to the Andreas Dillmann,Gerd Heller,Wolfgang Schr?der Conferen

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書目名稱New Results in Numerical and Experimental Fluid Mechanics VII
副標(biāo)題Contributions to the
編輯Andreas Dillmann,Gerd Heller,Wolfgang Schr?der
視頻videohttp://file.papertrans.cn/666/665731/665731.mp4
概述Recent results in Numerical and Experimental Fluid Mechanics.Presents new results in Aerospace in Germany.Written by experts in the field
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 VII; Contributions to the Andreas Dillmann,Gerd Heller,Wolfgang Schr?der Conferen
描述th This volume contains the papers presented at the 16 DGLR/STAB-Symposium held at the Eurogress Aachen and organized by RWTH Aachen University, Germany, November, 3 - 4, 2008. STAB is the German Aerospace Aerodynamics Association, founded towards the end of the 1970‘s, whereas DGLR is the German Society for Aeronautics and Astronautics (Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal Oberth e.V.). The mission of STAB is to foster development and acceptance of the discipline “Aerodynamics” in Germany. One of its general guidelines is to concentrate resources and know-how in the involved institutions and to avoid duplication in research work as much as possible. Nowadays, this is more necessary than ever. The experience made in the past makes it easier now, to obtain new knowledge for solving today‘s and tomorrow‘s problems. STAB unites German scientists and engineers from universities, research-establishments and industry doing research and project work in numerical and experimental fluid mechanics and aerodynamics for aerospace and other applications. This has always been the basis of numerous common research activities sponsored by different funding agencies. Since 198
出版日期Conference proceedings 2010
關(guān)鍵詞Aerodynamic Experimental Techniques; Aerodynamic Projects; Aerodynamics; Analytical Methods; Fluid Mecha
版次1
doihttps://doi.org/10.1007/978-3-642-14243-7
isbn_softcover978-3-642-42252-2
isbn_ebook978-3-642-14243-7Series ISSN 1612-2909 Series E-ISSN 1860-0824
issn_series 1612-2909
copyrightSpringer Berlin Heidelberg 2010
The information of publication is updating

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Prediction of the Wind Tunnel Sidewall Effect for the iGREEN Wing-Tailplane Interference Experimentde-wall. Results show that the effect of the sidewalls is similar to an offset in the angle of attack (but can only partially be corrected by a change in .), and that this effect is proportional to the lift and Mach number. These results were used in the design phase for the iGREEN wing-tailplane interference experiment.
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Application of the Immersed Boundary Method for the Simulation of Incompressible Flows in Complex anf this approach for flow simulations in complex and moving geometries are characterised. Simple validation test cases are addressed first, followed by a moving boundary example and more complex geometries like the Weibel lung model.
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New Results in Numerical and Experimental Fluid Mechanics VII978-3-642-14243-7Series ISSN 1612-2909 Series E-ISSN 1860-0824
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tors, frustrated with tedious and time-consuming decision-making—for example during single negotiation rounds—seek both general and mini-agreements, including framework agreements, and implement plans that intend to provide structures to the social relations and frameworks of future decisions. Never
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Giuseppe Bonfigli,Patrick Jennytors, frustrated with tedious and time-consuming decision-making—for example during single negotiation rounds—seek both general and mini-agreements, including framework agreements, and implement plans that intend to provide structures to the social relations and frameworks of future decisions. Never
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