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Rotary Balance Data for a Single Engine General Aviation Design Having a High Aspect-Ratio Canard for an Angle-of-Attack Range of 30Deg to 90Deg.

机译:单引擎通用航空设计的旋转平衡数据具有高纵横比的鸭翼,适用于30Deg至90Deg的攻角范围。

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摘要

Aerodynamic characteristics obtained in a helical flow environment utilizing a rotary balance located in the Langley spin tunnel are presented in plotted form. The configurations tested included the basic airplane, various control deflections, two canard locations, and wing leading edge modifications, as well as airplane components.

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