TY - GEN
T1 - Curved mesh generation using radial basis functions
AU - Kashi, Aditya
AU - Luo, Hong
N1 - Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2016
Y1 - 2016
N2 - A method for generating curved meshes from linear meshes is presented in this work. The method is designed to generate a curved mesh for any type of grid in a computationally inexpensive and numerically robust manner. In this method, high-order nodes are first placed in the linear mesh, the high-order boundary nodes are then relocated to the true boundary, and finally, the high-order interior nodes are moved using radial basis function (RBF) interpolation based on the motion of the high-order boundary nodes. The developed method is used to generate curved meshes for two- and three-dimensional geometries. The numerical experiments indicate that the RBF-interpolation method is much better than the prevalent linear-elasticity methods for generating high-order curved meshes judging by curved-mesh quality, computing cost, and ease of implementation.
AB - A method for generating curved meshes from linear meshes is presented in this work. The method is designed to generate a curved mesh for any type of grid in a computationally inexpensive and numerically robust manner. In this method, high-order nodes are first placed in the linear mesh, the high-order boundary nodes are then relocated to the true boundary, and finally, the high-order interior nodes are moved using radial basis function (RBF) interpolation based on the motion of the high-order boundary nodes. The developed method is used to generate curved meshes for two- and three-dimensional geometries. The numerical experiments indicate that the RBF-interpolation method is much better than the prevalent linear-elasticity methods for generating high-order curved meshes judging by curved-mesh quality, computing cost, and ease of implementation.
UR - http://www.scopus.com/inward/record.url?scp=85089160372&partnerID=8YFLogxK
U2 - 10.2514/6.2016-3179
DO - 10.2514/6.2016-3179
M3 - Conference contribution
AN - SCOPUS:85089160372
SN - 9781624104367
T3 - 46th AIAA Fluid Dynamics Conference
BT - 46th AIAA Fluid Dynamics Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 46th AIAA Fluid Dynamics Conference, 2016
Y2 - 13 June 2016 through 17 June 2016
ER -