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Titlebook: New Results in Numerical and Experimental Fluid Mechanics V; Contributions to the Hans-Josef Rath,Carsten Holze,Heinz Hönlinger Conference

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书目名称New Results in Numerical and Experimental Fluid Mechanics V
副标题Contributions to the
编辑Hans-Josef Rath,Carsten Holze,Heinz Hönlinger
视频video
概述All about new results in Aerospace in Germany
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 V; Contributions to the Hans-Josef Rath,Carsten Holze,Heinz Hönlinger Conference
描述.This volume contains the contributions to the 14. Symposium of the STAB (German Aerospace Aerodynamics Association). In this association all those German scientists and engineers from universities, research establishments and industry are involved, who are doing research and project work in numerical and experimental fluid mechanics and aerodynamics, mainly for aerospace but for other applications, too. Many of the contributions are presenting results from national and European Community sponsored projects. The volume gives a broad overview over the ongoing work in this field in Germany, with the topics being high-aspect ratio wings, low aspect-ratio wings, bluff bodies, laminar flow control and transition, active flow control, hypersonic flows, aeroelasticity, aeroacoustics, mathematical fundamentals/ numerical simulation, physical fundamentals, and facilities..
出版日期Conference proceedings 2006
关键词Aerodynamic Experimental Techniques; Aerodynamic Projects; Aerodynamics; Analytical Methods; Numerical M
版次1
doihttps://doi.org/10.1007/978-3-540-33287-9
isbn_softcover978-3-642-06995-6
isbn_ebook978-3-540-33287-9Series ISSN 1612-2909 Series E-ISSN 1860-0824
issn_series 1612-2909
copyrightSpringer-Verlag Berlin Heidelberg 2006
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Application of the PSP Technique in Low Speed Wind Tunnelsipped with two propeller simulators driven by pressurized air. The great challenge was to compensate the influence of the warm and cold air pipes which are guided inside the wing, creating large temperature differences on the models surface. The PSP (pressure sensitive paint) measurements were carri
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Aerodynamic Optimisation of a Flying Wing Transport Aircraftord length opfimisation. The applied finite volume flow solver is the DLR code FLOWer. The methods are described and results for a flying wing configuration are presented. The paper represents parts of DLR’s contribution to the aerodynamics work package of the VELA project, supported by European Com
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Computation of Delta Wing Flap Oscillations with a Reynolds-Averaged Navier-Stokes Solver test case is presented and compared to other numerical results. Having put the numerical method’s validity into evidence, the unsteady flow induced by an oscillating flap is investigated for a Fighter Type Delta Wing.
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