摘要: Active Flow Control (AFC) experiments performed at the Caltech Lucas Adaptive Wall Wind Tunnel on a 12%-thick, generic vertical tail model indicated that sweeping jets emanating from the trailing edge (TE) of the vertical stabiliz... 展开
作者 | E. Graff I. Wygnanski J. Lin R. Seele | ||
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原报告号 | N20130003329 | 总页数 | 18 |
主办者 | National Aeronautics and Space Administration | ||
报告分类号 | [51C - Aircraft] | ||
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Actuators Aircraft control Control surfaces Flapping Free flow Jet flow Lift devices Rudders Tail assemblies Trailing edges Yaw |