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Wind tunnel investigation of control surface characteristics XII : various cover-plate alinements on the NACA 0015 airfoil with a 30 percent chord flap and large sealed internal balance

机译：控制表面特性的风洞调查XII：NaCa 0015翼型上的各种盖板，三角翼和大密封内部平衡

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作者
Hoggard, H Page, Jr;
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年度 1943
页码 1-13
总页数 13
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
CONTROL SURFACES - CHARACTERISTICS; CONTROL SURFACES, BALANCED - HINGE MOMENTS WIND TUNNEL TESTS; WING FLAPS, BALANCED - INTERNAL; WING FLAPS, SEALED-GAP; AIRFOILS - NACA 0015-CHAR , MOMENTS & ORDINATES WING FLAPS,BALANCED - WING FLAPS; WING FLAPS - DEFLECTION; WING SPOILERS;

机译：控制表面 - 特征;控制表面，平衡 - 铰接式风洞测试;翼平衡，平衡 - 内部;翼襟翼，密封间隙; aIRFOILs - NaCa 0015-CHaR，mOmENTs＆amp;选择翼形翼片，平衡翼形翼片;翼片 - 挠曲; WING spOILERs;

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专利

1. Application of an AC barrier discharge actuator to control airflow separation above a NACA 0015 airfoil: Optimization of the actuation location along the chord [J] . Jolibois J, Forte M, Moreau E Journal of Electrostatics . 2008,第9a10期

机译：交流障碍放电致动器在控制NACA 0015机翼上方的气流分离中的应用：沿弦的致动位置的优化
2. Numerical and Experimental Investigations of Lift and Drag Performances of NACA 0015 Wind Turbine Airfoil [J] . ?zzet ?ahin, Adem Acir International Journal of Materials, Mechanics and Manufacturing . 2015,第1期

机译：NACA 0015风力机翼型升力和阻力性能的数值和实验研究
3. Lift characteristics of pitching NACA0015 airfoil due to unsteady forced surface inflation [J] . Heydari Ali, Pasandideh-Fard Mahmoud Journal of Mechanical Science and Technology . 2015,第6期

机译：由于不稳定的强制表面膨胀，俯仰NACA0015机翼的升力特性
4. Flow Control of a NACA 0015 Airfoil Using a Chordwise Array of Synthetic Jets [C] . K. Bales, R. Jefferies, U.S, Aerospace Sciences Meeting and Exhibit . 2003

机译：使用合成射流按弦排列的NACA 0015机翼的流量控制
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

机译：带有襟翼控制面并与机翼襟翼配合使用的无尾飞机的风洞测试。
6. Comparisons between LES and wind tunnel hot-wire measurements of a NACA 0015 airfoil [O] . Zhu Wei Jun, Shen Wen Zhong, Bertagnolio Franck, 2012

机译：LEs与NaCa 0015翼型的风洞热线测量之间的比较

Wind tunnel investigation of control surface characteristics XII : various cover-plate alinements on the NACA 0015 airfoil with a 30 percent chord flap and large sealed internal balance

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