| タイトル | Numerical simulation of viscous-inviscid interactions on indented nose tips |
| 著者（英） | Chaussee, D. S.; Mcrae, D. S.; Rizk, Y. M. |
| 著者所属（英） | NASA Ames Research Center|Dayton Univ. |
| 発行日 | 1982-01-01 |
| 言語 | eng |
| 内容記述 | An implicit numerical algorithm to solve the unsteady thin-layer Navier-Stokes equations in a strong conservative form has been used to compute the viscous flow over indented nose tips placed in a supersonic free stream. Numerical solutions are presented for axisymmetric and three-dimensional indented configurations for laminar flow conditions. Results demonstrate the capability of the present numerical procedure to predict flow fields that contain strong viscous-inviscid interactions, including boundary-layer separation, reattachment, and embedded discontinuities. Comparisons with available experimental data for the shock shape and surface pressure are also given. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 82A22084
AIAA PAPER 82-0290 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/411980 |
