| タイトル | An analysis of strake vortex breakdown characteristics in relation to design features |
| 著者（英） | Frink, N. T.; Lamar, J. E. |
| 著者所属（英） | NASA Langley Research Center|North Carolina State Univ. |
| 発行日 | 1980-01-01 |
| 言語 | eng |
| 内容記述 | This paper describes a water tunnel study of the vortex breakdown characteristics of a large number of analytically designed vortex strakes tested in combination with a moderate aspect ratio trapezoidal wing. A wide range of strake sizes and slenderness ratios are covered, and examples of the effects of the primary design parameters of size, span, and slenderness on the vortex breakdown characteristics are presented and analyzed in relation to the leading-edge suction distributions. Several examples of detailed planform shaping on strakes of the same general size and slenderness are shown from which it can be concluded that, consistent with the design criterion, those with leading-edge suction distributions which increase more rapidly near, and have a higher value at, the spanwise tip of the strake produce a more stable vortex. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 80A19320
AIAA PAPER 80-0326 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/423384 |
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