Abstract
An efficient edge based data structure has been developed in order to implement an unstructured vertex based finite volume algorithm for the Reynolds-averaged Navier–Stokes equations on hybrid meshes. In the present approach, the data structure is tailored to meet the requirements of the vertex based algorithm by considering data access patterns and cache efficiency. The required data are packed and allocated in a way that they are close to each other in the physical memory. Therefore, the proposed data structure increases cache performance and improves computation time. As a result, the explicit flow solver indicates a significant speed up compared to other open-source solvers in terms of CPU time. A fully implicit version has also been implemented based on the PETSc library in order to improve the robustness of the algorithm. The resulting algebraic equations due to the compressible Navier–Stokes and the one equation Spalart–Allmaras turbulence equations are solved in a monolithic manner using the restricted additive Schwarz preconditioner combined with the FGMRES Krylov subspace algorithm. In order to further improve the computational accuracy, the multiscale metric based anisotropic mesh refinement library PyAMG is used for mesh adaptation. The numerical algorithm is validated for the classical benchmark problems such as the transonic turbulent flow around a supercritical RAE2822 airfoil and DLR-F6 wing-body-nacelle-pylon configuration. The efficiency of the data structure is demonstrated by achieving up to an order of magnitude speed up in CPU times.
Original language | English |
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Pages (from-to) | 13-31 |
Number of pages | 19 |
Journal | International Journal for Numerical Methods in Fluids |
Volume | 94 |
Issue number | 1 |
DOIs | |
Publication status | Published - Jan 2022 |
Bibliographical note
Publisher Copyright:© 2021 John Wiley & Sons Ltd.
Funding
Computing Centre of the Slovak Academy of Sciences through PRACE, ITMS 26230120002 and 26210120002; Istanbul Technical University ‐ Scientific Research Project (ITU‐BAP), MGA‐2017‐40828; National Center for High Performance Computing of Turkey (UYBHM), 10752009; Scientific and Technical Research Council of Turkey (TUBITAK), TUBITAK ULAKBIM, High Performance and Grid Computing Center. Funding information The authors gratefully acknowledge the use of the computing resources provided by the National Center for High Performance Computing of Turkey (UYBHM) under grant number 10752009, the computing facilities at the High Performance and Grid Computing Center (TUBITAK ULAKBIM), and the PRACE‐Partnership for Advanced Computing in Europe (DECI‐16) resources through the Computing Centre of the Slovak Academy of Sciences supercomputing infrastructure acquired in project ITMS 26230120002 and 26210120002 (Slovak infrastructure for high‐performance computing) supported by the Research & Development Operational Programme funded by the ERDF. The authors also acknowledge partial financial support from Istanbul Technical University‐Scientific Research Project (ITU‐BAP) under project number MGA‐2017‐40828. The first author would like to acknowledge scholarship from Scientific and Technical Research Council of Turkey (TUBITAK).
Funders | Funder number |
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National Center for High Performance Computing of Turkey | |
UYBHM | 10752009 |
TUBITAK ULAKBIM | |
Slovenská Akadémia Vied | |
Türkiye Bilimsel ve Teknolojik Araştirma Kurumu | |
Partnership for Advanced Computing in Europe AISBL | ITMS 26230120002, 26210120002 |
TUBITAK | |
Istanbul Teknik Üniversitesi | MGA‐2017‐40828, ITU‐BAP |
UYBHM | 10752009 |
National Center for High Performance Computing of Turkey | |
TUBITAK ULAKBIM | |
Grid Computing Center | |
European Regional Development Fund | |
Türkiye Bilimsel ve Teknolojik Araştirma Kurumu | |
Istanbul Technical University‐Scientific Research Project | |
TUBITAK | |
ITU‐BAP | MGA‐2017‐40828 |
Keywords
- compressible flow
- computational aerodynamics
- data structures
- finite volume
- mesh adaptation
- Reynolds averaged Navier–Stokes