| タイトル | Aerothermal modeling program. Phase 2, element A: Improved numerical methods for turbulent viscous recirculating flows |
| 本文（外部サイト） | http://hdl.handle.net/2060/19890007932 |
| 著者（英） | Karki, K. C.; Patankar, Suhas V.; Mongia, H. C.; Runchal, A. K. |
| 著者所属（英） | General Motors Corp. |
| 発行日 | 1987-10-01 |
| 言語 | eng |
| 内容記述 | The objective of this effort is to develop improved numerical schemes for predicting combustor flow fields. Various candidate numerical schemes were evaluated, and promising schemes were selected for detailed assessment. The criteria for evaluation included accuracy, computational efficiency, stability, and ease of extension to multidimensions. The candidate schemes were assessed against a variety of simple one- and two-dimensional problems. These results led to the selection of the following schemes for further evaluation: flux spline schemes (linear and cubic) and controlled numerical diffusion with internal feedback (CONDIF). The incorporation of the flux spline scheme and direct solution strategy in a computer program for three-dimensional flows is in progress. |
| NASA分類 | FLUID MECHANICS AND HEAT TRANSFER |
| レポートNO | 89N17303 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/143381 |
|
