Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/5669
Title: Development of a pressure based, unstructured, GPU accelerated CFD solver for compressible reacting flows at all MACH numbers
Authors: Özkan, B.
Uslu, S.
Keywords: GPU acceleration
Numerical Combustion
Reactive Computational Fluid Dynamics RCFD
Issue Date: 2018
Publisher: International Conference on Computational Fluid Dynamics 2018
Source: 10th International Conference on Computational Fluid Dynamics, ICCFD 2018, 9 July 2018 through 13 July 2018, , 159583
Abstract: CFD, Computational Fluid Dynamics, tools have become an integral part of product design and analysis of gas turbines, rocket engines and thrusters. In order to model the chemical reacting flow in the combustion chambers, a CFD solver dealing with combustion of multi species reactions is developed. The solver must also be able to cope with the three flow regimes, subsonic, transonic and supersonic flow that occur in many flow problems. This is namely called a solver for all flow speeds. This solver also utilizes all resources of computers by being CPU parallel and GPU accelerated. A third party Open Source matrix solver ViennaCL is integrated to the Solver to solve linear system of equations. © ICCFD 2018.
URI: https://hdl.handle.net/20.500.11851/5669
Appears in Collections:Makine Mühendisliği Bölümü / Department of Mechanical Engineering
Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection

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