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Wind tunnel investigation of effect of wing location, power, and flap deflection on effective dihedral of a typical single-engine fighter-airplane model with tail removed

机译：机翼位置，动力和襟翼偏转对典型单引擎战斗机模型有效二面角影响的风洞研究

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Tucker, Warren A;
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年度 1946
页码 1-34
总页数 34
原文格式 PDF
正文语种 eng
中图分类工业技术;
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5. Wind tunnel test of a tailless aircraft with a belly-flap control surface used in combination with wing flaps. [D] . Dougherty, Daniel A. 2012

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7. Lift Enhancement of Ground-Effect Wing. 2nd Report. Experimental Investigation of the Power Augmented Ram Wing in Ground Effect through the Wind Tunnel. [O] . Takenori MATSUBARA, Masanori TASHIMO, Fumio KURE, 1992

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8. Wind-Tunnel Investigation of Effect of Wing Location, Power, and Flap Deflection on Effective Dihedral of a Typical Single-Engine Fighter-Airplane Model with Tail Removed [R] . Tucker, W. A. 1946

机译：翼位置，权力和襟翼偏转的影响对典型的单引擎战斗机，飞机与尾模型有效二面角风洞调查移除

Wind tunnel investigation of effect of wing location, power, and flap deflection on effective dihedral of a typical single-engine fighter-airplane model with tail removed

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