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Investigation of slat noise on high-lift configuration using active backscatter model in LES

Heitmann, Dirk and Ewert, Roland (2019) Investigation of slat noise on high-lift configuration using active backscatter model in LES. In: 25th AIAA/CEAS Aeroacoustics Conference, 2019. 25th AIAA/CEAS Aeroacoustics Conference, 20.-23. Mai 2019, Delft, Niederlande. doi: 10.2514/6.2019-2644.

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This contribution concerns the numerical prediction of high-lift wing slat noise. A zonal RANS-LES simulation was carried out. Within this approach active backscattering was realized to model the supplementary turbulent production caused by the non-resolved scales together with their turbulent scattering effect on the resolved wave-number scales. The CAA code solves the nonlinear Navier-Stokes equations utilizing Non-Linear Disturbance Equations (NLDE). The inclusion of active turbulent backscatter aims to provide a physical more complete subfilter forcing model as being possible with a purely dissipative model. This might help to reduce grid resolution requirements in Large Eddy Simulations (LES). The F16 wing geometry with deployed high-lift devices was used as testcase for this approach. The flow topology inside the slat cavity as well as the noise generation mechanisms are described and comparisons to experimental data are presented.

Item URL in elib:https://elib.dlr.de/129748/
Document Type:Conference or Workshop Item (Speech)
Title:Investigation of slat noise on high-lift configuration using active backscatter model in LES
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Date:May 2019
Journal or Publication Title:25th AIAA/CEAS Aeroacoustics Conference, 2019
Refereed publication:No
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:Large Eddy Simulation, subgrid scale model, active forcing
Event Title:25th AIAA/CEAS Aeroacoustics Conference
Event Location:Delft, Niederlande
Event Type:international Conference
Event Dates:20.-23. Mai 2019
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 - Simulation and Validation (old)
Location: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Technical Acoustics
Deposited By: Heitmann, Dirk
Deposited On:29 Oct 2019 14:03
Last Modified:18 Jul 2023 13:59

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