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Wind-tunnel investigation of aileron effectiveness of 0.20-airfoil-chord plain ailerons of true airfoil contour on NACA 65(sub 2)-415, 65(sub 3)-418 and 65(sub 4)-421 airfoil sections

机译：NaCa 65（sub 2）-415,65（sub 3）-418和65（sub 4）-421翼型截面上0.20-翼型平面副翼的真翼型轮廓副翼效能的风洞研究

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作者
Braslow, Albert L;
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年度 1944
页码 1-9
总页数 9
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AIRFOILS-NACA 652-415-CHAR & ORDINATES LOW-DRAG; AIRFOILS-NACA 653-418-CHAR & ORDINATES LOW-DRAG; AIRFOILS-NACA 654-421-CHAR & ORDINATES LOW-DRAG; AILERONS - EFFICIENCY; AILERONS, SEALED-GAP; AILERONS - DEFLECTION; WIND TUNNEL TESTS-NACA-PRESSURE, TWO-DIMENSIONAL (7 1/2' X 3');

机译：aIRFOILs-NaCa 652-415-CHaR＆amp; ORDINaTEs LOW-DRaG; aIRFOILs-NaCa 653-418-CHaR＆amp; ORDINaTEs LOW-DRaG; aIRFOILs-NaCa 654-421-CHaR＆amp; ORDINaTEs LOW-DRaG; aILERONs - 效率; aILERONs，sEaLED-Gap; aILERONs - DEFLECTION;风洞测试 - NaCa-pREssURE，二维（7 1/2'X 3'）;

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Wind-tunnel investigation of aileron effectiveness of 0.20-airfoil-chord plain ailerons of true airfoil contour on NACA 65(sub 2)-415, 65(sub 3)-418 and 65(sub 4)-421 airfoil sections

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