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Free-flight investigation to determine force and hinge-moment characteristics at zero angle of attack of a 60 degrees sweptback half-delta tip control on a 60 degrees sweptback delta wing at Mach numbers between 0.68 and 1.44

机译：自由飞行调查确定60度后掠三角翼控制在零度攻角下的力度和铰链力矩特性，在60度后掠三角翼上，马赫数在0.68和1.44之间

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Martz, C William; Church, James D; Goslee, John W;
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年度 1951
页码 1-38
总页数 38
原文格式 PDF
正文语种 eng
中图分类工业技术;
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6. Low speed aerodynamic characteristics of 60 degrees rounded leading-edge delta wing with vortex flaps [O] . Rinoie K. 1996

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Free-flight investigation to determine force and hinge-moment characteristics at zero angle of attack of a 60 degrees sweptback half-delta tip control on a 60 degrees sweptback delta wing at Mach numbers between 0.68 and 1.44

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