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Wind tunnel investigation of effect of yaw on lateral-stability characteristics IV : symmetrically tapered wing with a circular fuselage having a wedge-shaped rear and a vertical tail

机译：风洞对横向稳定特性影响的风洞研究IV：具有楔形后部和垂直尾翼的圆形机身的对称锥形机翼

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Wallace, Arthur R;
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年度 1942
页码 1-14
总页数 14
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
WINGS - STABILITY, LATERAL; ROLLING & YAWING MOMENTS - AIRFOILS - NACA 23012; WINGS, TAPERED - CHARACTERISTICS EFFECT OF WING FLAPS; FUSELAGES, CIRCULAR-WEDGE-SHAPED REAR; TAIL SURFACES, VERTICAL; INTERFERENCES - WINGS & FUSELAGES; MONOPLANES, MID-WING VS HIGH- & LOW-WING; STABILITY, DIRECTIONAL; WING FLAPS, SPLIT - PARTIAL-SPAN (20 CHORD);

机译：WINGs - sTaBILITY，LaTERaL;滚动＆amp; YaWING mOmENTs - aIRFOILs - NaCa 23012; WINGs，TapERED - 翼片的特征效应; FUsELaGEs，CIRCULaR-WEDGE-sHapED REaR; TaIL sURFaCEs，VERTICaL;干扰 - WINGs＆amp;机身; mONOpLaNEs，mID-WING Vs HIGH-＆amp; LOW-WING;稳定性，方向性;翼襟，分裂 - 部分跨度（20 CHORD）;

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Wind tunnel investigation of effect of yaw on lateral-stability characteristics IV : symmetrically tapered wing with a circular fuselage having a wedge-shaped rear and a vertical tail

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