Journal of Shanghai University(Natural Science Edition) ›› 2009, Vol. 15 ›› Issue (5): 464-469.
• Mathematics.Physics and Chemistry • Previous Articles Next Articles
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Abstract:
According to a mesh-free method based on total directional derivative, partial derivatives at all nodes and natural boundary conditions are constructed using the total directional derivative formula. Since no mesh/element is needed, it is simple both theoretically and computationally. The method is tested with a numerical example of compressible fluid flow. A reliable solution is obtained with high accuracy and efficiency.
Key words: mesh-free method; total directional derivative; flow past a two-dimensional airfoil; compressible flow
CLC Number:
O 354
LI Shi-Yu, CHEN Bo, LIU Gao-Lian, LU Zhan-Bin. A New Mesh-Free Difference Method Applied to Compressible Flow Past a Two-Dimensional Airfoil[J]. Journal of Shanghai University(Natural Science Edition), 2009, 15(5): 464-469.
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https://www.journal.shu.edu.cn/EN/Y2009/V15/I5/464