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Titlebook: New Results in Numerical and Experimental Fluid Mechanics XIII; Contributions to the Andreas Dillmann,Gerd Heller,Claus Wagner Conference p

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書目名稱New Results in Numerical and Experimental Fluid Mechanics XIII
副標(biāo)題Contributions to the
編輯Andreas Dillmann,Gerd Heller,Claus Wagner
視頻videohttp://file.papertrans.cn/666/665736/665736.mp4
概述Reports on cutting-edge fluid mechanics and aerodynamics research.Covers innovative applications in aeronautics, transportation, and energy.Focuses on both German and European projects
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 XIII; Contributions to the Andreas Dillmann,Gerd Heller,Claus Wagner Conference p
描述.This book offers timely insights into research on numerical and experimental fluid mechanics and aerodynamics, mainly for (but not limited to) aerospace applications. It reports on findings by members of the STAB (German Aerospace Aerodynamics Association) and DGLR (German Society for Aeronautics and Astronautics) and covers both nationally and EC-funded projects. Continuing on the tradition of the previous volumes, the book highlights innovative solutions, promoting translation from fundamental research to industrial applications. It addresses academics and professionals in the field of aeronautics, astronautics, ground transportation, and energy alike.. .?..?.
出版日期Conference proceedings 2021
關(guān)鍵詞Turbulent Flow Models; Wind tunnel model; Hybrid RANS/LENS model; Laminar Flow Control; Laminar Wing; Aer
版次1
doihttps://doi.org/10.1007/978-3-030-79561-0
isbn_softcover978-3-030-79563-4
isbn_ebook978-3-030-79561-0Series ISSN 1612-2909 Series E-ISSN 1860-0824
issn_series 1612-2909
copyrightThe Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Switzerl
The information of publication is updating

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Comparison of Different Methods for?the?Extraction of Airfoil Characteristics of Propeller Blades as.5d approach or via a recovery from the slipstream data, there is better agreement regarding thrust and slipstream velocities. Thereby, the 2.5d method shows a good compromise between computational effort and the quality of the results.
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Stochastic Modeling of Passive Scalars in?Turbulent Channel Flows: Predictive Capabilities of One-Dially resolve the boundary layer structure. Albeit the model is unable to capture the emerging dissimilarity of near-wall scalar and momentum transport for high ., it can economically and accurately represent fluctuating wall-normal fluxes.
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Conference proceedings 2021e solutions, promoting translation from fundamental research to industrial applications. It addresses academics and professionals in the field of aeronautics, astronautics, ground transportation, and energy alike.. .?..?.
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發(fā)表于 2025-3-22 23:05:59 | 只看該作者
1612-2909 vious volumes, the book highlights innovative solutions, promoting translation from fundamental research to industrial applications. It addresses academics and professionals in the field of aeronautics, astronautics, ground transportation, and energy alike.. .?..?.978-3-030-79563-4978-3-030-79561-0Series ISSN 1612-2909 Series E-ISSN 1860-0824
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Assessment of the Disturbance Velocity Approach to Determine the Gust Impact on Airfoils in TransoniVA. At higher angles of attack and a small gust wavelength, the DVA’s drag history shows deviations which should be taken into account. Overall, the DVA provides suitable results with respect to the resolved gust simulations.
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Study on Large-Scale Amplitude Modulation of Near-Wall Small-Scale Structures in Turbulent Wall-Bounn the resulting modal representations. The results show that the superposition effect and the amplitude modulation exist in all three velocity components but are most intense for the streamwise fluctuations. A high level of coherence of the sweeps and ejections is also detected by conventional cross-correlation.
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