| タイトル | Viscous hypersonic shock-on-shock interaction on blunt cowl lips |
| 著者（英） | Yee, H. C.; Klopfer, G. H. |
| 著者所属（英） | NASA Ames Research Center; Nielsen Engineering and Research, Inc. |
| 発行日 | 1988-01-01 |
| 言語 | eng |
| 内容記述 | The effects of impinging ramp shocks on a two-dimensional viscous inlet cowl of the National Aerospace Plane (NASP) or blunt body flow fields for various impingement locations are numerically simulated by a recently developed second-order implicit total variation diminishing (TVD) algorithm. The results demonstrate that accurate computation of heat transfer rate is crucially dependent on adequate normal grid resolution at the wall. The various numerical results are compared with recent experimental data. Due to the complex flow patterns that occur for the shock-on-shock flows, adaptive grid procedures are utilized. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 88A22175
AIAA PAPER 88-0233 |
| 権利 | Copyright |
