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Wind tunnel tests of ailerons at various speeds IV : ailerons of 0.20 airfoil chord and true contour with 0.35 aileron-chord extreme blunt-nose balance on the NACA 23012 airfoil

机译：不同速度副翼的风洞试验IV：NaCa 23012翼型上的0.20翼型弦和真正轮廓的副翼，具有0.35副翼弦极端钝头平衡

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作者
Anderson, R A;
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年度 1943
页码 1-17
总页数 17
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
LIFT CURVES - SLOPE; CONTROL STICKS - FORCES; FLYING, HIGH-SPEED; WIND TUNNEL TESTS - NACA - STABILITY; AILERONS, BALANCED - HINGE MOMENTS; MACH NUMBER; PRESSURE DISTRIBUTION - AIRFOILS - NACA 23012; AILERONS, BALANCED - SEALED-GAP; AIRFOILS - NACA 23012 - CHAR & MOMENTS; AILERONS - WIND TUNNEL TESTS;

机译：升降曲线 - 斜率;控制棒 - 力量;飞行，高速;风洞测试 - NaCa - 稳定性; aILERONs，BaLaNCED - HINGE mOmENTs;马赫数;压力分布 - 翼型 - NaCa 23012; aILERONs，BaLaNCED - sEaLED-Gap; aIRFOILs - NaCa 23012 - CHaR＆amp; mOmENTs; aILERONs - 风洞隧道测试;

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1. Numerical and Experimental Wind Tunnel and Flight Testing of Active Flow Control for Modified NACA 64_3-618 Airfoil [C] . James V. Dianics, Duncan M. Ohno, Stefan D. Fuggmann, AIAA aerospace sciences meeting;AIAA SciTech forum . 2015

机译：改进的NACA 64_3-618翼型主动流控制的数值和实验风洞和飞行试验
2. Wind tunnel tests of the NACA 63-415 and a modified NACA 63-415 airfoil [O] . Bak C., Fuglsang P., Johansen J., 2000

机译：NaCa 63-415和改进的NaCa 63-415翼型的风洞试验

Wind tunnel tests of ailerons at various speeds IV : ailerons of 0.20 airfoil chord and true contour with 0.35 aileron-chord extreme blunt-nose balance on the NACA 23012 airfoil

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