TILDA: Towards Industrial LES/DNS in Aeronautics -

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
Buch | Hardcover
IX, 550 Seiten
2021 | 1st ed. 2021
Springer International Publishing (Verlag)
978-3-030-62047-9 (ISBN)
235,39 inkl. MwSt

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. 

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.

Erscheinungsdatum
Reihe/Serie Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Zusatzinfo IX, 550 p. 344 illus., 273 illus. in color.
Verlagsort Cham
Sprache englisch
Maße 155 x 235 mm
Gewicht 997 g
Themenwelt Technik Maschinenbau
Schlagworte Curved mesh generation • discontinuous Galerkin • Dual time stepping • Flux Reconstruction • H2020 TILDA projects • High-order CFD methods • High-performance computing in aeronautics • High Reynolds Number Flows • Implicit time integration methods • LES Applications • Multigrid multilevel preconditioners • Runge-Kutta methods
ISBN-10 3-030-62047-6 / 3030620476
ISBN-13 978-3-030-62047-9 / 9783030620479
Zustand Neuware
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