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Wind-tunnel investigation of control-surface characteristics XVII : beveled-trailing-edge flaps of 0.20, 0.30, and 0.40 airfoil chord on an NACA 0009 airfoil

机译：控制面特性的风洞研究XVII：NaCa 0009翼型上0.20,0.30和0.40翼型弦的斜边 - 后缘襟翼

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作者
Lockwood, Vernard E;
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年度 1944
页码 1-53
总页数 53
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
CONTROL SURFACES-CHARACTERISTICS; WING FLAPS-EFFECT OF GAPS; WING FLAPS-HINGE MOMENTS; WING FLAPS, SEALED-GAP; WING FLAPS, BEVELED; AIRFOILS-NACA 0009-CHAR , MOMENTS & ORDINATES WING FLAPS; WING FLAPS-DEFLECTION;

机译：控制表面 - 特征;翼隙 - Gaps效应; WING FLaps-HINGE mOmENTs;翼襟翼，密封间隙;翼襟翼，被瞄准; aIRFOILs-NaCa 0009-CHaR，mOmENTs＆amp;选择翼襟翼; WING FLaps-DEFLECTION;

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Wind-tunnel investigation of control-surface characteristics XVII : beveled-trailing-edge flaps of 0.20, 0.30, and 0.40 airfoil chord on an NACA 0009 airfoil

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