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Wind-tunnel investigation at low speed of the lateral control characteristics of an unswept untapered semi-span wing of aspect ratio 3.13 equipped with various 25-percent-chord plain ailerons

机译：风速隧道调查低速侧向控制特性的未纵横的半跨翼纵横比3.13配备各种25％弦平原副翼

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Johnson, Harold S; Hagerman, John R;
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年度 1950
页码 1-35
总页数 35
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AILERON CONTROLS; WINGS - CHARACTERISTICS; AILERONS - HINGE MOMENTS; WIND TUNNEL TESTS - NACA - 300 MPH (10 FEET X 7 FEET); AILERONS - DEFLECTION; AIRFOILS - NACA 64A010; AILERONS - POSITION; ROLLING, PITCHING & YAWING MOMENTS - WINGS;

机译：aILERON CONTROLs;翅膀 - 特征; aILERONs - HINGE mOmENTs;风洞隧道测试 - NaCa - 300英里/小时（10英尺X 7英尺）; aILERONs - DEFLECTION; aIRFOILs - NaCa 64a010; aILERONs - pOsITION; ROLLING，pITCHING＆amp; YaWING mOmENTs - WINGs;

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Wind-tunnel investigation at low speed of the lateral control characteristics of an unswept untapered semi-span wing of aspect ratio 3.13 equipped with various 25-percent-chord plain ailerons

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