摘要: Studies have been made on several wing leading-edge modifications applicable at present to single-engine light aircraft, which produce stabilizing vortices at stall and beyond. These vortices have the effect of fixing the stall pa... 展开
作者 | Feistel, T. W. Anderson, S. B. Kroeger, R. A. | ||
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原报告号 | N19980202341 | 总页数 | 8 |
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 | Separated flow Boundary layer separation Wings Aerodynamic stalling Wind tunnel tests Angle of attack Leading edges Roll Lift Vortices Light aircraft Aircraft landing Flight envelopes Flow visualization Yawing moments Approach |