Özet
An efficient edge based data structure has been proposed for the implementation of vertex based finite volume formulation. In the present approach, the quad-edge and halfedge data structures are redesigned and simplified in order to fit requirements of the cell-vertex centered finite volume methods. The present data structure is not limited with triangles, arbitrary polygons are also supported in the mesh without putting any additional effort. An explicit second-order compressible Euler solver based on the present data structure has been implemented in order to demonstrate its efficiency compared to the classical edge-based implementation for a vertex based finite volume formulation. Nevertheless, a fully implicit version of the present numerical algorithm has also been implemented based on PETSc library in order to improve the robustness of the algorithm. As a benchmark problem, the calculations over an RAE2822 airfoil and a circular cylinder are performed in order to demonstrate its efficiency.
Orijinal dil | İngilizce |
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Ana bilgisayar yayını başlığı | 23rd AIAA Computational Fluid Dynamics Conference, 2017 |
Yayınlayan | American Institute of Aeronautics and Astronautics Inc, AIAA |
ISBN (Basılı) | 9781624105067 |
DOI'lar | |
Yayın durumu | Yayınlandı - 2017 |
Etkinlik | 23rd AIAA Computational Fluid Dynamics Conference, 2017 - Denver, United States Süre: 5 Haz 2017 → 9 Haz 2017 |
Yayın serisi
Adı | 23rd AIAA Computational Fluid Dynamics Conference, 2017 |
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???event.eventtypes.event.conference??? | 23rd AIAA Computational Fluid Dynamics Conference, 2017 |
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Ülke/Bölge | United States |
Şehir | Denver |
Periyot | 5/06/17 → 9/06/17 |
Bibliyografik not
Publisher Copyright:© 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.