A Hybrid Cartesian-Body Fitted Grid Approach for Simulations of Fluid Flows in Complex Geometries
Xiangying Chen, Gecheng Zha
Abstract
Xiangying Chen, Gecheng Zha
Abstract
A novel approach of automated hybrid Cartesian-body fltted grid (HCBFG) for simulations of ∞uid ∞ows in complex geometries is suggested. Based on a Cartesian background grid, the new approach automatically searches a near wall boundary(NWB) at any instant when a geometry is given. Within the NWB, a body-fltted mesh is generated using an e‐cient algebraic method with the skew angle between any two mesh lines guaranteed between 45 ‐ and 135 ‐ . This is attributed to the fact that only the mesh lines tangential to the solid surface needs to be generated. The mesh lines in the other two directions are from the background Cartesian grid. Outside of the NWB, the Cartesian grid is used. On the NWB, the grid points are one-to-one connected with the Cartesian grid. Hence, a consistent discretization scheme for structured grid can be used with no interpolation needed at the NWB. The fully conservative ∞ux calculation can be achieved. This new approach has the advantages of the Chimera grid and Cartesian grid methods to treat complex or moving geometry, but overcomes the drawbacks of those methods requiring interpolation on the difierent mesh boundaries. Beneflted from the HCBFG, all the rigorous numerical techniques developed for body-fltted grid, which are essential to achieve high order accuracy, can be used. The mesh size of the proposed hybrid grid approach will also be substantially smaller than that of a Cartesian grid method or unstructured grids since a highly stretched grid can be used near walls. This new approach may open a door to a new class of CFD technique for e‐ciently and accurately simulating steady and unsteady ∞ows, furthermore, solving moving grid and ∞uid-structural interaction problems with complex geometries. This paper presents several examples of the HCBFG for representative geometries. The transonic RAE2822 airfoil is calculated using an implicit line Gauss-Seidel iteration to demonstrate the feasibility of the method.
OpenAlex reports 3 citations for this work. Citation counts describe recorded attention and do not establish research quality.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
A novel approach of automated hybrid Cartesian-body fltted grid (HCBFG) for simulations of ∞uid ∞ows in complex geometries is suggested. Based on a Cartesian background grid, the new approach automatically searches a near wall boundary(NWB) at any instant when a geometry is given. Within the NWB, a body-fltted mesh is generated using an e‐cient algebraic method with the skew angle between any two mesh lines guaranteed between 45 ‐ and 135 ‐ . This is attributed to the fact that only the mesh lines tangential to the solid surface needs to be generated. The mesh lines in the other two directions are from the background Cartesian grid. Outside of the NWB, the Cartesian grid is used. On the NWB, the grid points are one-to-one connected with the Cartesian grid. Hence, a consistent discretization scheme for structured grid can be used with no interpolation needed at the NWB. The fully conservative ∞ux calculation can be achieved. This new approach has the advantages of the Chimera grid and Cartesian grid methods to treat complex or moving geometry, but overcomes the drawbacks of those methods requiring interpolation on the difierent mesh boundaries. Beneflted from the HCBFG, all the rigorous numerical techniques developed for body-fltted grid, which are essential to achieve high order accuracy, can be used. The mesh size of the proposed hybrid grid approach will also be substantially smaller than that of a Cartesian grid method or unstructured grids since a highly stretched grid can be used near walls. This new approach may open a door to a new class of CFD technique for e‐ciently and accurately simulating steady and unsteady ∞ows, furthermore, solving moving grid and ∞uid-structural interaction problems with complex geometries. This paper presents several examples of the HCBFG for representative geometries. The transonic RAE2822 airfoil is calculated using an implicit line Gauss-Seidel iteration to demonstrate the feasibility of the method.
Key concepts: Cartesian coordinate system, Grid, Computer science, Regular grid, Computational science, Mesh generation, Solid modeling, Unstructured grid