摘要: An investigation has been made in the Langley 20-foot free-spinning tunnel to determine the erect and inverted spin and recovery characteristics of a 1/30-scale dynamic model of a twin-jet swept-wing fighter airplane. The model re... 展开
作者 | Bowman, J. S. Healy, F. M. | ||
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原报告号 | N19980223580 | 总页数 | 22 |
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 | Aircraft spin Control stability Spin dynamics Wind tunnel tests Wind tunnel models Aerodynamic stalling Fighter aircraft Scale models Swept wings Aircraft stability Aircraft performance Aircraft safety Aerodynamic drag Aerodynamic coefficients Ailerons Rudders |