| タイトル | An improved higher order panel method for linearized supersonic flow |
| 著者（英） | Epton, M. A.; Magnus, A. E.; Rubbert, P. E.; Ehlers, F. E.; Johnson, F. T. |
| 著者所属（英） | Boeing Commercial Airplane Co. |
| 発行日 | 1978-01-01 |
| 言語 | eng |
| 内容記述 | An improved higher order panel method for linearized supersonic flow is described. Each panel, defined by four points on the surface, is divided into eight subpanels in such a way that all subpanel and panel edges are contiguous. By prescribing a quadratic distribution of the doublet on each subpanel, the doublet strength is made strictly continuous on the paneled surface. A linear source distribution is also used. Numerical results are smoother and in better agreement with experiment than the previous method with less strict continuity. A brief discussion of superinclined panels used to eliminate interior interference in nacelles is included. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 78A52628
AIAA PAPER 78-15 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/430946 |
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