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Horizontal-tail effectiveness and downwash surveys for two 47.7 degree sweptback wing-fuselage combinations with aspect ratios of 5.1 and 6.0 at a Reynolds number of 6.0 x 10(exp 6).

机译：雷诺数为6.0 x 10（exp 6）的两个47.7度后掠翼 - 机身组合的水平尾效率和下洗调查，纵横比为5.1和6.0。

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Salmi, Reino J;
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年度 1951
页码 1-70
总页数 70
原文格式 PDF
正文语种 eng
中图分类工业技术;
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5. Some experiments on the flow in the boundary layer of a 45 degrees sweptback untapered wing of aspect ratio 4 [O] . Emslie K., Hosking L., Marshall W. S. D. 1953

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6. Effects of leading-edge devices and trailing-edge flaps on longitudinal characteristics of two 47.7 degree sweptback wings of aspect ratios 5.1 and 6.0 at a Reynolds number of 6.0 x 10(exp 6) [R] . Salmi, Reino J 1950

机译：雷诺数为6.0 x 10（exp 6）时，前缘装置和后缘襟翼对长宽比为5.1和6.0的两个47.7度后掠翼的纵向特性的影响

Horizontal-tail effectiveness and downwash surveys for two 47.7 degree sweptback wing-fuselage combinations with aspect ratios of 5.1 and 6.0 at a Reynolds number of 6.0 x 10(exp 6).

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