摘要: The spin and recovery characteristics of a 1/13-scale model of the NASA AD-1 oblique-wing research aircraft at wing-skew positions of 0, 25, 45, and 60 deg (right wing forward) were investigated. Spins were obtained for all wing-s... 展开
作者 | White, W. L. Bowman, J. S. | ||
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原报告号 | N8218183 | 总页数 | 28 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Aircraft spin Oblique wings Scale models Spin stabilization Wind tunnel tests Aerial rudders Aerodynamic stability Ailerons Attitude control Deflection Spin dynamics Spin tests |