摘要: Spanwise blowing over the wing and canard of a 1:35 model of a close-coupled-canard fighter airplane configuration (similar to the Kfir-C2) was investigated experimentally in low-speed flow. Tests were conducted at airspeeds of 30... 展开
作者 | Seginer, A. Salomon, M. | ||
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原报告号 | N83-22159 | 总页数 | 29 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Aircraft performance Aircraft stability Fighter aircraft Lift augmentation Spanwise blowing Aircraft maneuvers Angle of attack Delta wings Directional stability Lateral stability Leading edges Vortices Wind tunnel tests |