| タイトル | Convergence Acceleration for Multistage Time-Stepping Schemes |
| 本文（外部サイト） | http://hdl.handle.net/2060/20060022551 |
| 著者（英） | Swanson, R. C.; Vasta, V. N.; Rossow, C-C; Turkel, Eli L. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2006-01-01
2006 |
| 言語 | eng |
| 内容記述 | The convergence of a Runge-Kutta (RK) scheme with multigrid is accelerated by preconditioning with a fully implicit operator. With the extended stability of the Runge-Kutta scheme, CFL numbers as high as 1000 could be used. The implicit preconditioner addresses the stiffness in the discrete equations associated with stretched meshes. Numerical dissipation operators (based on the Roe scheme, a matrix formulation, and the CUSP scheme) as well as the number of RK stages are considered in evaluating the RK/implicit scheme. Both the numerical and computational efficiency of the scheme with the different dissipation operators are discussed. The RK/implicit scheme is used to solve the two-dimensional (2-D) and three-dimensional (3-D) compressible, Reynolds-averaged Navier-Stokes equations. In two dimensions, turbulent flows over an airfoil at subsonic and transonic conditions are computed. The effects of mesh cell aspect ratio on convergence are investigated for Reynolds numbers between 5.7 x 10(exp 6) and 100.0 x 10(exp 6). Results are also obtained for a transonic wing flow. For both 2-D and 3-D problems, the computational time of a well-tuned standard RK scheme is reduced at least a factor of four. |
| NASA分類 | Aerodynamics |
| レポートNO | AIAA Paper 2006-3523 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
|
