Burnazzi, Marco and Probst, Axel and Steger, Mathias (2019) Hybrid RANS/LES of an isolated engine nacelle with side wind using an unstructured CFD solver. In: Progress in Hybrid RANS-LES Modelling, 143, pp. 347-356. Springer International Publishing. 7th Symposium on Hybrid RANS-LES Methods, 17.-19. Sep. 2018, Berlin, Deutschland. doi: 10.1007/978-3-030-27607-2_28. ISBN 978-3-030-27606-5. ISSN 1612-2909.
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Official URL: https://doi.org/10.1007/978-3-030-27607-2_28
Abstract
The present work focuses on the scale-resolving numerical simulation of an isolated jet-engine intake in presence of side wind. The computation was carried out with the DLR TAU code within the framework of the Rolls-Royce funded project FaNcI (Fan-Nacelle Integration) and relied on advanced numerical techniques recently developed as part of the DLR project VicToria (Virtual Aircraft Technology Integration Platform). The goal of the present work was the simulation of the intake flow in off-design condition with high crosswind: a partially separated flow where the flow reattachment takes place in the proximity of the hypothetical fan location. A hybrid RANS/LES method based on the Improved Delayed Detached-Eddy Simulation (IDDES) was combined with the low-dispersion low-dissipation numerical scheme (LD2). In particular, a hybrid formulation of the LD2 scheme ensured robustness also in regions of complex grid topologies and flow phenomena involving strong gradients. The result validation is based on experimental measurements of the flow distortion inside the engine inlet. From the final picture the need for scale-resolving turbulence simulation and the advantage of a specific numerical scheme clearly emerge.
Item URL in elib: | https://elib.dlr.de/119628/ | ||||||||||||||||||
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Document Type: | Conference or Workshop Item (Speech) | ||||||||||||||||||
Additional Information: | Print ISBN 978-3-030-27606-5 Online ISBN 978-3-030-27607-2 | ||||||||||||||||||
Title: | Hybrid RANS/LES of an isolated engine nacelle with side wind using an unstructured CFD solver | ||||||||||||||||||
Authors: |
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Date: | 2 November 2019 | ||||||||||||||||||
Journal or Publication Title: | Progress in Hybrid RANS-LES Modelling | ||||||||||||||||||
Refereed publication: | Yes | ||||||||||||||||||
Open Access: | Yes | ||||||||||||||||||
Gold Open Access: | No | ||||||||||||||||||
In SCOPUS: | No | ||||||||||||||||||
In ISI Web of Science: | Yes | ||||||||||||||||||
Volume: | 143 | ||||||||||||||||||
DOI : | 10.1007/978-3-030-27607-2_28 | ||||||||||||||||||
Page Range: | pp. 347-356 | ||||||||||||||||||
Editors: |
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Publisher: | Springer International Publishing | ||||||||||||||||||
Series Name: | Notes on Numerical Fluid Mechanics and Multidisciplinary Design | ||||||||||||||||||
ISSN: | 1612-2909 | ||||||||||||||||||
ISBN: | 978-3-030-27606-5 | ||||||||||||||||||
Status: | Published | ||||||||||||||||||
Keywords: | CFD, Hybrid RANS-LES, Engine Nacelle, Turbulence modeling | ||||||||||||||||||
Event Title: | 7th Symposium on Hybrid RANS-LES Methods | ||||||||||||||||||
Event Location: | Berlin, Deutschland | ||||||||||||||||||
Event Type: | international Conference | ||||||||||||||||||
Event Dates: | 17.-19. Sep. 2018 | ||||||||||||||||||
HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||
HGF - Program: | Aeronautics | ||||||||||||||||||
HGF - Program Themes: | fixed-wing aircraft | ||||||||||||||||||
DLR - Research area: | Aeronautics | ||||||||||||||||||
DLR - Program: | L AR - Aircraft Research | ||||||||||||||||||
DLR - Research theme (Project): | L - VicToria (old) | ||||||||||||||||||
Location: | Göttingen | ||||||||||||||||||
Institutes and Institutions: | Institute for Aerodynamics and Flow Technology > CASE, GO | ||||||||||||||||||
Deposited By: | Probst, Axel | ||||||||||||||||||
Deposited On: | 07 Nov 2018 17:18 | ||||||||||||||||||
Last Modified: | 11 Dec 2019 18:36 |
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