摘要: A wind-tunnel investigation was conducted in the Langley 12-Foot Low-Speed Tunnelto study the low-speed stability and control characteristics of a series of four flying wings over an extended range of angle of attack (-8 deg to 48... 展开
作者 | Ross, H. M. Fears, S. P. Moul, T. M. | ||
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原报告号 | N9613037 | 总页数 | 144 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Angle of attack Arrow wings Dynamic characteristics Low aspect ratio wings Low speed Radar cross sections Sideslip Tailless aircraft Wind tunnel tests Aspect ratio Lateral control Lateral stability Leading edge flaps Longitudinal stability T |