TY - GEN
T1 - A novel efficient reconstruction scheme for unstructured grids based on iterative least-squares methods
AU - Tamaki, Yoshiharu
AU - Imamura, Taro
N1 - Funding Information:
This research is funded by JSPS KAKENHI Grant Number 15H05559 (Grant-in-Aid for Young Scientists (A)).
Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2016
Y1 - 2016
N2 - A new compact higher-order variable reconstruction scheme based on iterative least-squares methods is proposed. The approximation of derivatives is split into multi-step first-order least-squares methods, and then converges to higher-order values through iteration. The scheme is defined only by the values stored in the face-adjacent cells. The size of the stencils and reconstruction matrix, and thus the computational cost and memory consumption is significantly reduced. In a time-evolutional problem, the converged value at the previous time-step is used as an initial value of the iteration in order to achieve quick convergence. In addition, a WENO-like weight function is implemented for shock-capturing problems. In a vortex-advection problem, it is shown that only one iteration of the reconstruction per time-step gives sufficient convergence, and that higher-order accuracy is achieved efficiently. Then a double-Mach reflection problem is simulated. The present scheme shows high resolution of the unsteady flow structure, and no severe numerical instability is observed. The computational cost of the fourth-order iterative reconstruction is cheaper than the conventional k -exact reconstruction with the same order of accuracy.
AB - A new compact higher-order variable reconstruction scheme based on iterative least-squares methods is proposed. The approximation of derivatives is split into multi-step first-order least-squares methods, and then converges to higher-order values through iteration. The scheme is defined only by the values stored in the face-adjacent cells. The size of the stencils and reconstruction matrix, and thus the computational cost and memory consumption is significantly reduced. In a time-evolutional problem, the converged value at the previous time-step is used as an initial value of the iteration in order to achieve quick convergence. In addition, a WENO-like weight function is implemented for shock-capturing problems. In a vortex-advection problem, it is shown that only one iteration of the reconstruction per time-step gives sufficient convergence, and that higher-order accuracy is achieved efficiently. Then a double-Mach reflection problem is simulated. The present scheme shows high resolution of the unsteady flow structure, and no severe numerical instability is observed. The computational cost of the fourth-order iterative reconstruction is cheaper than the conventional k -exact reconstruction with the same order of accuracy.
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U2 - 10.2514/6.2016-1100
DO - 10.2514/6.2016-1100
M3 - Conference contribution
AN - SCOPUS:85007415747
SN - 9781624103933
T3 - 54th AIAA Aerospace Sciences Meeting
BT - 54th AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 54th AIAA Aerospace Sciences Meeting, 2016
Y2 - 4 January 2016 through 8 January 2016
ER -