CHINESE JOURNAL OF COMPUTATIONAL PHYSICS ›› 2016, Vol. 33 ›› Issue (3): 266-272.

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Moving Mesh Method for Pitching Naca0012 Airfoil

ZENG Xianyang1, NI Guoxi2   

  1. 1. Graduate School of China Academy of Engineering Physics, Beijing 100088, China;
    2. Laboratory of Computational Physics, Institute of Applied Physics and Computational Mathematics, Beijing 100088, China
  • Received:2015-03-19 Revised:2015-05-31 Online:2016-05-25 Published:2016-05-25

Abstract: We give discretization for fluid system in integral form with arbitrary moving velocity on unstructured meshes, where re-mapping step in ALE method to interpolate flow variables between old mesh and new one can be avoided. We give three kinds of velocity for different part of computational domain, and apply the scheme to pitching Naca0012 airfoil with moving boundary. It shows that the scheme is efficient and accurate.

Key words: compressible fluid system, moving boundary, pitching Naca0012, adaptive moving mesh method

CLC Number: