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- W2569734172 abstract "Cartesian grids constitute a special branch in unstructured grid technology. They use specially designed algorithms to generate automatic grids for complex geometries and to simulate flows around such geometries regardless of the body shape and number of bodies. Cartesian grids are generated by constructing a quadtree based data structure for the purpose of connecting the Cartesian cells to each other. A “hands-off”, Cartesian grid generator based Euler solution called GeULER is implemented in object-oriented FORTRAN programming language. In this study, implementations of generated two-dimensional adaptive refinement/coarsening scheme codesare appended to the developed compressible flow solver by using special Cartesian-based algorithms, namely cut-cell adaptation and curvature adaptation around BOEING TR-1322 multi-element airfoil. A subsonic flow at free stream Mach number of 0.11 around the airfoil is tested to predict pressure distributions around it and Mach contours of the flow are depicted by using the developed GeULER code." @default.
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- W2569734172 date "2015-07-28" @default.
- W2569734172 modified "2023-10-18" @default.
- W2569734172 title "BOEING TR-1322 Çoklu-elemanlı Kanat Profili Çevresinde Sıkıştırılabilir Akış için Çözüm Uyarlamalı Kartezyen Ağ Temelli Euler Çözümü" @default.
- W2569734172 doi "https://doi.org/10.17100/nevbiltek.210947" @default.
- W2569734172 hasPublicationYear "2015" @default.
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