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Effect of vertical location of a horizontal tail on the static longitudinal stability characteristics of a 45 degree sweptback-wing-fuselage combination of aspect ratio 8 at a Reynolds number of 4.0 x 10(exp 6)

机译：水平尾翼的垂直位置对雷诺数为4.0 x 10（exp 6）的45度后掠翼机身纵横比8组合的静态纵向稳定性特性的影响

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Salmi, Reino J; Jacques, William A;
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年度 1952
页码 1-49
总页数 49
原文格式 PDF
正文语种 eng
中图分类工业技术;
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Effect of vertical location of a horizontal tail on the static longitudinal stability characteristics of a 45 degree sweptback-wing-fuselage combination of aspect ratio 8 at a Reynolds number of 4.0 x 10(exp 6)

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