| タイトル | Experimental study of the vortex flow behavior on a generic fighter wing at subsonic and transonic speeds |
| 著者（英） | Erickson, Gary E.; Rogers, Lawrence W. |
| 著者所属（英） | NASA Ames Research Center; Air Force Wright Aeronautical Labs. |
| 発行日 | 1987-06-01 |
| 言語 | eng |
| 内容記述 | A subsonic and transonic investigation of the vortex flow behavior of a generic fighter configuration with 55-deg cropped delta wing has been conducted in order to improve current understanding of vortical motions on a wing with deflected leading edge flap at moderate and high angles-of-attack. The leading edge vortex strength was reduced, and the vortex was flatter and closer to the wing surface, as the Mach number increased. Transonically, at high angles-of-attack, the test data suggested the development of a cross-flow shock wave above the vortex sheet which coexisted with a rear shock wave. Subsonically, a deflected leading edge flap was able to sustain a concentrated vortex on the forward-facing surface. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 87A44920
AIAA PAPER 87-1262 |
| 権利 | Copyright |
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