Fr. 238.00

TILDA: Towards Industrial LES/DNS in Aeronautics - Paving the Way for Future Accurate CFD - Results of the H2020 Research Project TILDA, Funded by the European Union, 2015 -2018

Inglese · Copertina rigida

Spedizione di solito entro 2 a 3 settimane (il titolo viene stampato sull'ordine)

Descrizione

Ulteriori informazioni

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. 

Sommario

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.

Dettagli sul prodotto

Con la collaborazione di Sergey Bosniakov (Editore), Jean-Francois Boussuge (Editore), Frederic Chalot (Editore), Vincent Couaillier (Editore), Werner Haase (Editore), Ralf Hartmann (Editore), Ralf Hartmann et al (Editore), Koe Hillewaert (Editore), Koen Hillewaert (Editore), Charles Hirsch (Editore)
Editore Springer, Berlin
 
Lingue Inglese
Formato Copertina rigida
Pubblicazione 25.12.2020
 
EAN 9783030620479
ISBN 978-3-0-3062047-9
Pagine 550
Dimensioni 179 mm x 37 mm x 242 mm
Illustrazioni IX, 550 p. 344 illus., 273 illus. in color.
Serie Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Categoria Scienze naturali, medicina, informatica, tecnica > Tecnica > Meccanica, tecnica di produzione

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