摘要: An investigation has been conducted in the Langley spin tunnel to determine the spin and recovery characteristics of a 1/20-scale model of the Northrop F-5E airplane. The investigation included erect and inverted spins, a range of... 展开
作者 | Scher, S. H. White, W. L. | ||
---|---|---|---|
原报告号 | N19980227417 | 总页数 | 48 |
主办者 | National Aeronautics and Space Administration | ||
报告分类号 | [51A - Aerodynamics] | ||
报告类别/文献类型 | DE / NTIS科技报告 | ||
关键词 | F-5 aircraft Scale models Wind tunnel tests Aircraft spin Spin dynamics Control stability Aircraft control Aircraft performance Aircraft safety Controllability Maneuvers External stores Trailing edge flaps Moments of inertia |