| タイトル | Computation of three-dimensional, inviscid supersonic flows |
| 著者（英） | Kutler, P. |
| 著者所属（英） | NASA Ames Research Center |
| 発行日 | 1975-01-01 |
| 言語 | eng |
| 内容記述 | The paper sets forth in detail a method for the finite-difference computation of three-dimensional supersonic fields in an Eulerian mesh. First-, second-, and third-order finite difference schemes are examined. Attention is given to proper treatment of the impermeable and permeable boundaries encompassing the computational plane. Numerical results are presented for certain specific configurations: a conical wing-body combination, internal corner flow, a two-dimensional blunt body, an interfering shock problem, and three-dimensional inviscid supersonic flow past a shuttle-orbiter type vehicle. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 76A22955 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/443999 |
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