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Evaluation of the Noise Reduction Potential of a Krueger Flap High-Lift device via the Lattice Boltzmann Method

Soni, Malav Mukesh and Ewert, Roland and Dierke, Jürgen and Delfs, Jan Werner (2023) Evaluation of the Noise Reduction Potential of a Krueger Flap High-Lift device via the Lattice Boltzmann Method. In: AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023. American Institute of Aeronautics and Astronautics, Inc. AIAA AVIATION 2023 Forum, 2023-06-12 - 2023-06-16, San Diego, USA. doi: 10.2514/6.2023-4477. ISBN 978-162410704-7. ISSN 6.2023-4477.

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Official URL: https://arc.aiaa.org/doi/abs/10.2514/6.2023-4477

Abstract

Main objective of this work is to conduct Direct Noise Computation of high-lift wings using wall-modeled LES with LBM. For this purpose, we employ an industrial LBM software ProLB. In our previously reported work, we presented a quantitatively successful validation of a conventional high-lift wing (DLR/ONERA F16). This study carries forward our high-lift noise investigation, now with a Krueger flap as an alternative high-lift device that has been proposed elsewhere for the laminar wing concepts. Aeroacoustically, in the absence of noise-generating mechanisms that are typically present at the conventional slat i.e. interacting and impinging shear layers, this design provides a potential for noise reduction. For this study, we use two different Krueger flap designs: reference and aerodynamically optimized Krueger. Reference Krueger has a short chord while the optimized Krueger has a long chord. These multi-element, unswept high-lift wings with deployed Krueger flap and flap are resolved on a mesh with 5%clean chord length spanwise extent. Periodic boundary condition is applied along the spanwise direction. For the relative accuracy, the time-averaged near field WM-LES results for both the Krueger flap variants are compared with the RANS. Far field acoustic comparison is carried out between the conventional slat (F16) and both the Krueger leading edge devices. Optimized Krueger shows a noise reduction potential over the reference Krueger and conventional slat based design. Further noise reduction potential is observed when the cavity for Krueger flap to stow back is closed in the simulation. It is found that the stowage cavity contributes to the overall noise radiation for frequencies higher than 3 kHz. Additional improvement towards tackling of the periodicity effect in the direct noise computation of high-lift approaches is reported. Periodicity introduces a cut-on type jump in the pressure spectrum. A new approach is introduced for the specific spanwise periodic setup that cancels excess energy induced by the additional cut-on modes.

Item URL in elib:https://elib.dlr.de/200742/
Document Type:Conference or Workshop Item (Speech)
Title:Evaluation of the Noise Reduction Potential of a Krueger Flap High-Lift device via the Lattice Boltzmann Method
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Soni, Malav MukeshMalav.Soni (at) dlr.dehttps://orcid.org/0009-0006-1013-1495217926374
Ewert, RolandRoland.Ewert (at) dlr.dehttps://orcid.org/0009-0004-4331-041XUNSPECIFIED
Dierke, JürgenJuergen.Dierke (at) dlr.deUNSPECIFIEDUNSPECIFIED
Delfs, Jan WernerJan.Delfs (at) dlr.dehttps://orcid.org/0000-0001-8893-1747149013805
Date:8 June 2023
Journal or Publication Title:AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI:10.2514/6.2023-4477
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
Soni, Malav MukeshMalav.Soni (at) dlr.dehttps://orcid.org/0009-0006-1013-1495217926374
Ewert, RolandRoland.Ewert (at) dlr.dehttps://orcid.org/0009-0004-4331-041XUNSPECIFIED
Dierke, JürgenJuergen.Dierke (at) dlr.deUNSPECIFIEDUNSPECIFIED
Delfs, Jan WernerJan.Delfs (at) dlr.dehttps://orcid.org/0000-0001-8893-1747149013805
Publisher:American Institute of Aeronautics and Astronautics, Inc
ISSN:6.2023-4477
ISBN:978-162410704-7
Status:Published
Keywords:Krueger, High-lift noise, LBM, WM-LES, Noise reduction
Event Title:AIAA AVIATION 2023 Forum
Event Location:San Diego, USA
Event Type:international Conference
Event Start Date:12 June 2023
Event End Date:16 June 2023
Organizer:American Institute of Aeronautics and Astronautics, Inc.
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Virtual Aircraft and  Validation, L - Aircraft Technologies and Integration
Location: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Technical Acoustics
Deposited By: Soni, Malav Mukesh
Deposited On:19 Dec 2023 12:07
Last Modified:17 Jun 2026 11:27

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