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Towards CFD-based Aeroelastic Analysis of the CRM-NLF wing

Helm, Sebastian and Fehrs, Michael and Kaiser, Christoph and Krimmelbein, Normann and Krumbein, Andreas (2021) Towards CFD-based Aeroelastic Analysis of the CRM-NLF wing. AIAA Aviation Forum, 02.-06. Aug. 2021, virtuell. doi: 10.2514/6.2021-2503.

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Official URL: https://arc.aiaa.org/doi/abs/10.2514/6.2021-2503

Abstract

The natural laminar flow wing CRM-NLF shows promising numerical and experimental results. This work aims at understanding the aerodynamic characteristics of the CRM-NLF wing under wind-tunnel conditions. The focus of the present paper is put on the impact of static aeroelastic deformation of the model. Furthermore, the effect of turbulent wedges is shown to be significant. Fluid-structure coupled simulations show an impoved agreement with wind-tunnel data made available by NASA when both effects are considered.

Item URL in elib:https://elib.dlr.de/146682/
Document Type:Conference or Workshop Item (Speech)
Title:Towards CFD-based Aeroelastic Analysis of the CRM-NLF wing
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Helm, SebastianSebastian.Helm (at) dlr.dehttps://orcid.org/0000-0001-5483-0884
Fehrs, MichaelMichael.Fehrs (at) dlr.deUNSPECIFIED
Kaiser, ChristophChristoph.Kaiser (at) dlr.dehttps://orcid.org/0000-0001-9156-8352
Krimmelbein, Normannnormann.krimmelbein (at) dlr.deUNSPECIFIED
Krumbein, AndreasAndreas.Krumbein (at) dlr.dehttps://orcid.org/0000-0002-2772-7328
Date:28 July 2021
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.2514/6.2021-2503
Status:Published
Keywords:Laminar wing, CFD-CSM coupling, static aeroelastic deformation, turbulent wedges
Event Title:AIAA Aviation Forum
Event Location:virtuell
Event Type:international Conference
Event Dates:02.-06. Aug. 2021
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L - no assignment
DLR - Research theme (Project):L - no assignment
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Aeroelastic Simulation
Institute for Aerodynamics and Flow Technology > CASE, BS
Institute for Aerodynamics and Flow Technology > CASE, GO
Deposited By: Helm, Sebastian
Deposited On:02 Dec 2021 16:43
Last Modified:22 Feb 2022 18:25

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