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The damping in roll of rocket-powered test vehicles having rectangular wings with NACA 65-006 and symmetrical double-wedge airfoil sections of aspect ratio 4.5

机译：具有NaCa 65-006矩形机翼和纵横比为4.5的对称双楔翼型截面的火箭动力试验车的阻尼

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Dietz, Albert E; Edmondson, James L;
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年度 1950
页码 1-14
总页数 14
原文格式 PDF
正文语种 eng
中图分类工业技术;
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2. Numerical studies influence configuration fairing flap track airfoil type naca 4412 and naca 6412 character unmanned aerial vehicle (UAV) [J] . Handrico Ramelan Pratama, Muhammad Agung Bramantya MATEC Web of Conferences . 2018,第12期

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3. Comparison of the Aerodynamic Characteristics of the NACA0012 Airfoil at Low-to-Moderate Reynolds Numbers for any Aspect Ratio [J] . S. Martínez-Aranda, A. L. García-González, L. Parras, International Journal of Aerospace Sciences . 2016,第1期

机译：在任何纵横比下，中低雷诺数下NACA0012机翼的空气动力学特性比较
4. COMPUTATIONS OF AERODYNAMIC BEHAVIOUR OF RECTANGULAR WING WITH NACA653218AIRFOIL [C] . Eslam Said Abdelghany, Osama E. Abdellatif, Gamal elhariry, AIAA aerospace sciences meeting;AIAA SciTech Forum . 2016

机译：用NACA653218机翼计算矩形机翼的气动行为。
5. A model for roll stall and the inherent stability modes of low aspect ratio wings at low Reynolds numbers. [D] . Shields, Matt. 2014

机译：低雷诺数下的低失速比机翼侧倾失速和固有稳定性模式的模型。
6. Numerical studies influence configuration fairing flap track airfoil type naca 4412 and naca 6412 character unmanned aerial vehicle (UAV) [O] . Handrico Ramelan Pratama, Muhammad Agung Bramantya 2018

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The damping in roll of rocket-powered test vehicles having rectangular wings with NACA 65-006 and symmetrical double-wedge airfoil sections of aspect ratio 4.5

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