A hybrid mesh free local RBF-Cartesian FD scheme for incompressible flow around solid bodies

A method for simulating flow around the solid bodies has been presented using hybrid meshfree and mesh-based schemes. The presented scheme optimizes the computational efficiency by combining the advantages of both meshfree and mesh-based methods. In this approach, a cloud of meshfree nodes has been...

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Bibliographic Details
Main Authors: Javed, A. (Author), Djidjeli, K. (Author), Xing, J.T (Author), Cox, S.J (Author)
Format: Article
Language:English
Published: 2013-09.
Subjects:
Online Access:Get fulltext
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100 1 0 |a Javed, A.  |e author 
700 1 0 |a Djidjeli, K.  |e author 
700 1 0 |a Xing, J.T.  |e author 
700 1 0 |a Cox, S.J.  |e author 
245 0 0 |a A hybrid mesh free local RBF-Cartesian FD scheme for incompressible flow around solid bodies 
260 |c 2013-09. 
856 |z Get fulltext  |u https://eprints.soton.ac.uk/359003/1/IJCEVol7%252810%25292013.pdf 
520 |a A method for simulating flow around the solid bodies has been presented using hybrid meshfree and mesh-based schemes. The presented scheme optimizes the computational efficiency by combining the advantages of both meshfree and mesh-based methods. In this approach, a cloud of meshfree nodes has been used in the domain around the solid body. These meshfree nodes have the ability to efficiently adapt to complex geometrical shapes. In the rest of the domain, conventional Cartesian grid has been used beyond the meshfree cloud. Complex geometrical shapes can therefore be dealt efficiently by using meshfree nodal cloud and computational efficiency is maintained through the use of conventional mesh-based scheme on Cartesian grid in the larger part of the domain. Spatial discretization of meshfree nodes has been achieved through local radial basis functions in finite difference mode (RBF-FD). Conventional finite difference scheme has been used in the Cartesian 'meshed' domain. Accuracy tests of the hybrid scheme have been conducted to establish the order of accuracy. Numerical tests have been performed by simulating two dimensional steady and unsteady incompressible flows around cylindrical object. Steady flow cases have been run at Reynolds numbers of 10, 20 and 40 and unsteady flow problems have been studied at Reynolds numbers of 100 and 200. Flow Parameters including lift, drag, vortex shedding, and vorticity contours are calculated. Numerical results have been found to be in good agreement with computational and experimental results available in the literature. 
655 7 |a Article