| タイトル | Flowfield in the plane of symmetry below a delta wing |
| 著者（英） | Seebass, A. R.; Cramer, M. S.; George, A. R. |
| 著者所属（英） | Cornell Univ. |
| 発行日 | 1976-02-01 |
| 言語 | eng |
| 内容記述 | The flowfield in the plane of symmetry of a thin lifting delta wing with supersonic leading edges is examined for wings with apex angles that are comparable to the Mach angle, as well as for the limiting case of a straight leading edge. For these two cases, a simplified treatment of the interaction between the plane expansion wave emanating from the trailing edge and the three-dimensional bow shock is presented. In the region unaffected by the wing tips, the shock decays inversely with distance from the wing. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 76A31180 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/443316 |
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