Deng, S. orcid.org/0000-0003-1324-4541, Wang, Y. and Qin, N. orcid.org/0000-0002-6437-9027 (2023) Cross-field structured adaptive mesh using medial axis flow feature extraction. AIAA Journal. ISSN 0001-1452
Abstract
A method to generate feature-aligned anisotropic structured meshes automatically is presented for high resolution of two-dimensional complicated flow features such as normal and oblique shock waves, shock reflection, shock/shock interaction, and shock/boundary-layer interaction. The method starts from extraction of dominant flow features to be treated alongside geometric entities. This is followed by automatic generation of multiblock structured meshes of the flow domain using a cross-field based method so that the flow feature entities are embedded along with the geometries. The cross-field method allows for the automatic blocking so that anisotropic quadrilateral meshes generation and adaptation to resolve flow features can be carried out. The resulting mesh possesses high element quality for orthogonality and high resolution of the flow features, suitable for the shock capturing methods and higher-order reconstruction schemes. The method is demonstrated through a number of aerodynamic flow test cases with discussion on its efficiency, accuracy, and robustness.
Metadata
Item Type: | Article |
---|---|
Authors/Creators: |
|
Copyright, Publisher and Additional Information: | © 2023 The Authors. Except as otherwise noted, this author-accepted version of a journal article published in AIAA Journal is made available via the University of Sheffield Research Publications and Copyright Policy under the terms of the Creative Commons Attribution 4.0 International License (CC-BY 4.0), which permits unrestricted use, distribution and reproduction in any medium, provided the original work is properly cited. To view a copy of this licence, visit http://creativecommons.org/licenses/by/4.0/ |
Keywords: | Computational Fluid Dynamics; Drag Coefficient; Hierarchical Adaptive Mesh Refinement; Structured Adaptive Mesh Refinement; shock boundary layer interaction; shock interaction; cross-field method; medial axis method; feature aligned mesh |
Dates: |
|
Institution: | The University of Sheffield |
Academic Units: | The University of Sheffield > Faculty of Engineering (Sheffield) > Department of Mechanical Engineering (Sheffield) |
Depositing User: | Symplectic Sheffield |
Date Deposited: | 31 Oct 2023 16:09 |
Last Modified: | 31 Oct 2023 16:09 |
Status: | Published |
Publisher: | American Institute of Aeronautics and Astronautics (AIAA) |
Refereed: | Yes |
Identification Number: | 10.2514/1.j063346 |
Related URLs: | |
Open Archives Initiative ID (OAI ID): | oai:eprints.whiterose.ac.uk:204784 |