摘要: An investigation has been conducted with a free-flying radio-controlled 0.13-scale model of a twin-jet swept-wing fighter airplane to determine the tendency of this design to enter spins and to evaluate the nature of the spin obta... 展开
作者 | Burk, S. M. Libbey, C. E. | ||
---|---|---|---|
原报告号 | N19980223579 | 总页数 | 42 |
主办者 | National Aeronautics and Space Administration | ||
报告分类号 | [51A - Aerodynamics51C - Aircraft] | ||
报告类别/文献类型 | DE / NTIS科技报告 | ||
关键词 | Fighter aircraft Aircraft spin Spin dynamics Aerodynamic stalling Wind tunnel tests Wind tunnel models Scale models Swept wings Control stability Maneuvers Aircraft stability Aircraft performance Ailerons Rudders Gyration Controllability |