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Transonic flutter investigation of a cantilevered, aspect-ratio-4, 45 degree sweptback, untapered wing with three different pylon-mounted external store configurations

机译：跨音速颤振调查悬臂，纵横比-4,45度后掠，非锥形翼与三个不同的塔架安装外部存储配置

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Ruhlin, Charle L; Bowwinkle, Robert W , Jr;
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年度 1957
页码 1-37
总页数 37
原文格式 PDF
正文语种 eng
中图分类工业技术;
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入库时间 2022-08-29 11:19:19

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机译：二维机翼-襟翼-尾翼构造对跨音速襟翼，尾翼颤动和极限周期振动的非线性气动影响
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机译：储存数量对三角翼配置的跨音速颤振特性的影响
5. Flutter suppression of wings with external stores using shape memory alloys [D] . Le, Anne H. 2007

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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

机译：锥形比对一系列薄悬臂机翼的横向振荡特性的一些效果，其具有45°的扫频角和纵横比4.0

Transonic flutter investigation of a cantilevered, aspect-ratio-4, 45 degree sweptback, untapered wing with three different pylon-mounted external store configurations

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