elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Accessibility | Contact | Deutsch
Fontsize: [-] Text [+]

Algorithms for Geometry-Adapted Mesh Refinement with Cell Stack Preservation in the FlowSimulator

Höchel, Maximilian and Hafemann, Thomas and Orlt, Matthias and Sanchez Ortiz, Roberto Iker (2025) Algorithms for Geometry-Adapted Mesh Refinement with Cell Stack Preservation in the FlowSimulator. Conference for Adaptive Mesh Refinement and Applications 2025 (AMR 25), 2025-09-02 - 2025-09-04, Köln, Deutschland. (Unpublished)

[img] PDF
2MB

Abstract

Adaptive mesh refinement allows Computational-Fluid-Dynamics (CFD) simulations to obtain faster solutions with more accuracy. However, given a refinement indicator field, a pure threshold-based refinement of individual cells is not enough. Under refinement, the boundary of the mesh has to converge to the true geometry, while high-quality boundary layer meshes must be maintained for high-Reynolds-number flows. Here we propose a FlowSimulator-based in-memory process chain for geometry-adapted mesh refinement with cell-stack-preservation. The process chain can seamlessly be integrated into previous CFD scenarios, since it deals with existing meshes and geometries without requiring control over the meshing process. It combines the FlowSimulator DataManager (FSDM) with several FlowSimulator plug-ins, including the high-order, highly-parallelized CFD Software by ONERA, DLR and Airbus (CODA). This work focuses on the plug-ins for mesh refinement, FSAdaptationNG, and Computational Aided Design (CAD) based geometry-handling, FSOCCT. FSAdaptationNG is a volume-cell-driven hierarchical nonconforming mesh refinement tool for fully unstructured storage. It is designed to satisfy the requirements of FlowSimulator in general and CODA in particular. To be applicable to CFD-simulations with boundary layers, it features cell stack-oriented refinement. FSOCCT gives access to some functionalities of the CAD-kernel Open CASCADE Technology (OCCT) to the FlowSimulator. In addition, it implements a meta-data-based mapping between mesh objects and the CAD model. By using vendor-neutral CAD-formats and mesh formats available in the FSDM, it is independent of a specific modeling or meshing tool, and works with the available meta-data using similarities between the hierarchical structure of CAD models and meshes with defined boundary conditions. The reliability of the process chain is demonstrated by application to test cases from the aerospace industry. Results showed that geometry-adapted mesh refinement with cell-stack preservation enables recovering the original geometry during refinement.

Item URL in elib:https://elib.dlr.de/216488/
Document Type:Conference or Workshop Item (Speech)
Title:Algorithms for Geometry-Adapted Mesh Refinement with Cell Stack Preservation in the FlowSimulator
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Höchel, Maximilianmaximilian.hoechel (at) dlr.dehttps://orcid.org/0000-0002-4195-1529UNSPECIFIED
Hafemann, ThomasThomas.Hafemann (at) dlr.deUNSPECIFIEDUNSPECIFIED
Orlt, MatthiasMatthias.Orlt (at) dlr.deUNSPECIFIEDUNSPECIFIED
Sanchez Ortiz, Roberto IkerRoberto.SanchezOrtiz (at) dlr.dehttps://orcid.org/0009-0004-1945-152XUNSPECIFIED
Date:3 September 2025
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Unpublished
Keywords:Computational Fluid Dynamics, Adaptive Mesh Refinement, CAD geometry, Mesh Deformation
Event Title:Conference for Adaptive Mesh Refinement and Applications 2025 (AMR 25)
Event Location:Köln, Deutschland
Event Type:international Conference
Event Start Date:2 September 2025
Event End Date:4 September 2025
Organizer:Dr. Johannes Holke
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 - Digital Technologies
Location: Dresden , Göttingen
Institutes and Institutions:Institute of Software Methods for Product Virtualization > High Perfomance Computing
Institute of Software Methods for Product Virtualization > Simulation Frameworks
Institute for Aerodynamics and Flow Technology > CASE, GO
Deposited By: Höchel, Maximilian
Deposited On:22 Sep 2025 09:05
Last Modified:22 Sep 2025 09:05

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
OpenAIRE Validator logo electronic library is running on EPrints
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.