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Roll-Control Effectiveness, of Several Spoiler Configurations on an Airplane Model with Wing Sweep of 55 Deg and 75 Deg at Supersonic Mach Numbers

机译：在超音速马赫数下机翼扫描为55度和75度的飞机模型上的几种扰流器配置的侧倾控制效果

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作者
Hayes, C.;
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作者单位

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年度 1971
页码 1-6
总页数 6
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Aircraft models ; Lateral control ; Spoilers ; Supersonic flow ; Variable sweep wings ; Aerodynamics ; Angle of attack ; Reynolds number;

机译：飞机模型;横向控制;扰流板;超音速流;可变扫掠翼;空气动力学;迎角;雷诺数;

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6. Roll-control effectiveness, of several spoiler configurations on an airplane model with wing sweep of 55 deg and 75 deg at supersonic Mach numbers [R] . Hayes, C. 1971

机译：在超音速马赫数下机翼扫描为55度和75度的飞机模型上的几种扰流器配置的侧倾控制效果

Roll-Control Effectiveness, of Several Spoiler Configurations on an Airplane Model with Wing Sweep of 55 Deg and 75 Deg at Supersonic Mach Numbers

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