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Low-speed pressure-distribution investigation of a spoiler and a spoiler-slot-deflector on a 30 degree sweptback wing-fuselage model having an aspect ratio of 3, a taper ratio of 0.5, and NACA 65A004 airfoil section

机译：30度后掠翼 - 机身模型上扰流板和扰流板 - 导流板的低速压力分布调查，纵横比为3，锥度比为0.5，NaCa 65a004翼型截面

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Hammond, Alexander D;
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年度 1956
页码 1-177
总页数 177
原文格式 PDF
正文语种 eng
中图分类工业技术;
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6. Some Effects of Taper Ratio on the Transonic Flutter Characteristics of a Series of Thin Cantilever Wings Having a Sweptback Angle of 45° and an Aspect Ratio 4.0 [O] . Eiichi NAKAI, Toshiro TAKAGI, Yasukatsu ANDO 1966

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Low-speed pressure-distribution investigation of a spoiler and a spoiler-slot-deflector on a 30 degree sweptback wing-fuselage model having an aspect ratio of 3, a taper ratio of 0.5, and NACA 65A004 airfoil section

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