| タイトル | Multigrid acceleration of the flux split Euler equations |
| 著者（英） | Anderson, W. K.; Thomas, J. L.; Whitfield, D. L. |
| 著者所属（英） | NASA Langley Research Center; Mississippi State Univ. |
| 発行日 | 1986-01-01 |
| 言語 | eng |
| 内容記述 | Multigrid acceleration is applied to a flux-split algorithm for solving the Euler equations in two and three dimensions. The basic algorithm is an implicit spatially-split approximate factorization method. The stability of the scheme in comparison to other factorization is examined. Results are presented for two-dimensional airfoil flows and three-dimensional wing flows which demonstrate substantially improved convergence with the multigrid algorithm. An asymptotic spectral radius of 0.89 and 0.93 is attained for a 97 x 17 x 17 wing solution at subcritical and supercritical conditions, respectively. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 86A19784
AIAA PAPER 86-0274 |
| 権利 | Copyright |
