Charles Hirsch & Koen Hillewaert 
TILDA: Towards Industrial LES/DNS in Aeronautics [PDF ebook] 
Paving the Way for Future Accurate CFD – Results of the H2020 Research Project TILDA, Funded by the European Union, 2015 -2018

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This book offers detailed insights into new methods for high-fidelity CFD, and their industrially relevant applications in aeronautics. It reports on the H2020 TILDA project, funded by the European Union in 2015-2018. The respective chapters demonstrate the potential of high-order methods for enabling more accurate predictions of non-linear, unsteady flows, ensuring enhanced reliability in CFD predictions.


The book highlights industrially relevant findings and representative test cases on the development of high-order methods for unsteady turbulence simulations on unstructured grids; on the development of the LES/DNS methodology by means of multilevel, adaptive, fractal and similar approaches for applications on unstructured grids; and on leveraging existent large-scale HPC networks to facilitate the industrial applications of LES/DNS in daily practice. Furthermore, the book discusses multidisciplinary applications of high-order methods in the area of aero-acoustics. All in all, it offers timely insights into the application and performance of high-order methods for CFD, and an extensive reference guide for researchers, graduate students, and industrial engineers whose work involves CFD and turbulence modeling. 

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表中的内容

The TILDA Project – Objectives, Project and Activities.- Implicit methods.- Multi-level approach.- Space Adaptive Methods/Meshing.- Wall-modelled LES.- Quality Measures for Curvilinear Finite Elements.- Parallelisation to Several Tens-of-thousands of cores.- I/O post- and Co-processing for High-order Methods.- Implementation of High Order Discontinuous Galerkin Method and its Verification using Taylor-Green Vortex and Periodic Hills Test Cases.- Large Eddy Simulation of single stream jet using High-order methods.- Boeing Rudimentary Landing Gear Configurations.- Generic Falcon Business Jet in Landing Configuration.- Detached-Eddy Simulation of Dual Stream Nozzle Jet Using High Order Discontinuous Galerkin Method.

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语言 英语 ● 格式 PDF ● 网页 550 ● ISBN 9783030620486 ● 文件大小 22.6 MB ● 编辑 Charles Hirsch & Koen Hillewaert ● 出版者 Springer International Publishing ● 市 Cham ● 国家 CH ● 发布时间 2021 ● 下载 24 个月 ● 货币 EUR ● ID 7878394 ● 复制保护 社会DRM

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