| タイトル | Numerical solution to the glancing sidewall oblique shock wave/turbulent boundary layer interaction in three dimension |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830013928 |
| 著者（英） | Benson, T. J.; Anderson, B. H. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1983-01-01 |
| 言語 | eng |
| 内容記述 | A supersonic three-dimensional viscous forward-marching computer design code called PEPSIS is used to obtain a numerical solution of the three-dimensional problem of the interaction of a glancing sidewall oblique shock wave and a turbulent boundary layer. Very good results are obtained for a test case that was run to investigate the use of the wall-function boundary-condition approximation for a highly complex three-dimensional shock-boundary layer interaction. Two additional test cases (coarse mesh and medium mesh) are run to examine the question of near-wall resolution when no-slip boundary conditions are applied. A comparison with experimental data shows that the PEPSIS code gives excellent results in general and is practical for three-dimensional supersonic inlet calculations. |
| NASA分類 | AIRCRAFT PROPULSION AND POWER |
| レポートNO | 83N22199
E-1521
AIAA PAPER 83-0136
NAS 1.15:83056
NASA-TM-83056 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/162941 |
