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Two-Dimensional Wind-Tunnel Tests of a Jet-Type Spoiler on an Naca 64A010 Airfoil Section Equipped with High-Lift Devices

机译：在Naca 64a010翼型截面上配备高升力装置的喷射式扰流板的二维风洞试验

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作者
Ballentine, D. C.; Barnard, G. A.;
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年度 1954
页码 p.1-10
总页数 10
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Airfoils; Jets; Spoilers; Aerodynamic characteristics; Model tests; Wind tunnel models;

机译：翼型;喷气式飞机;扰流板;空气动力学特性;模型试验;风洞模型;

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2. Aerodynamic Characteristics of High-Lift Devices with Downward Deflection of Spoiler [J] . Xiao-liang Wang, Fu-xin Wang, Ya-lin Li Journal of Aircraft . 2011,第2期

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3. Numerical efficiency evaluation of a vertical axis turbine equipped with 4 digits and 5 digits NACA airfoils [J] . Florina Costea, Ion Malael E3S Web of Conferences . 2019,第1期

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4. Flutter Study of NACA 64A010 Airfoil Using URANS and e~N Transition Models Coupled with an Integral Boundary Layer Code [C] . Ferran Marti, Feng Liu AIAA Aerospace Sciences Meeting;AIAA SciTech Forum . 2017

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6. Two-Dimensional Wind-Tunnel Tests of a Jet-Type Spoiler on an Naca 64A010 Airfoil Section Equipped with High-Lift Devices. [R] . Ballentine, D. C., Barnard, G. A. 1954

机译：一个喷流式扰流板的上NaCa 64a010翼剖面二维风洞试验配备了高升力装置。

Two-Dimensional Wind-Tunnel Tests of a Jet-Type Spoiler on an Naca 64A010 Airfoil Section Equipped with High-Lift Devices

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