TY - GEN
T1 - A fourth order accurate cellwise relaxation implicit disconstinuous galerkin scheme for solving RANS equations
AU - Asada, Hiroyuki
AU - Yasue, Kanako
AU - Ogino, Yousuke
AU - Sawada, Keisuke
PY - 2015/1/1
Y1 - 2015/1/1
N2 - A fourth order accurate Discontinuous Galerkin (DG) method coupled with cellwise relaxation implicit (CRI) scheme for solving the RANS equations is presented. Our efforts are focused on reducing computational time needed for setting Jacobian matrix. It is shown that the computational efficiency of the fourth order accurate DG-CRI scheme is substantially improved by employing several numerical techniques. Among the techniques, a use of the quadrature simplification by orthogonality is highly recommended in terms of the performance in reducing computational cost, numerical instability and required memory size. In the calculation of the turbulent boundary layer flow over a flat plate, it is shown that the quadrature simplification by orthogonality successfully reduces the computational time per step to 1/20. In the calculation of the vortical flowfield over a delta wing, the favorable spatial accuracy of the present fourth order accurate DG-CRI scheme is well demonstrated.
AB - A fourth order accurate Discontinuous Galerkin (DG) method coupled with cellwise relaxation implicit (CRI) scheme for solving the RANS equations is presented. Our efforts are focused on reducing computational time needed for setting Jacobian matrix. It is shown that the computational efficiency of the fourth order accurate DG-CRI scheme is substantially improved by employing several numerical techniques. Among the techniques, a use of the quadrature simplification by orthogonality is highly recommended in terms of the performance in reducing computational cost, numerical instability and required memory size. In the calculation of the turbulent boundary layer flow over a flat plate, it is shown that the quadrature simplification by orthogonality successfully reduces the computational time per step to 1/20. In the calculation of the vortical flowfield over a delta wing, the favorable spatial accuracy of the present fourth order accurate DG-CRI scheme is well demonstrated.
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U2 - 10.2514/6.2015-0057
DO - 10.2514/6.2015-0057
M3 - Conference contribution
AN - SCOPUS:84980348064
SN - 9781624103438
T3 - 53rd AIAA Aerospace Sciences Meeting
BT - 53rd AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 53rd AIAA Aerospace Sciences Meeting, 2015
Y2 - 5 January 2015 through 9 January 2015
ER -