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美国政府科技报告
>Effect of leading-edge high-lift devices and split flaps on the maximum-lift and lateral characteristics of a rectangular wing of aspect ratio 3.4 with circular-arc airfoil sections at Reynolds numbers from 2.9 x 10(exp 6) to 8.4 x 10(exp 6).
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Effect of leading-edge high-lift devices and split flaps on the maximum-lift and lateral characteristics of a rectangular wing of aspect ratio 3.4 with circular-arc airfoil sections at Reynolds numbers from 2.9 x 10(exp 6) to 8.4 x 10(exp 6).
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机译：前缘高升力装置和分离襟翼对纵横比为3.4的矩形机翼的最大升力和横向特性的影响，雷诺数为2.9 x 10（exp 6）至8.4 x 10的圆弧翼型截面exp 6）。
