Wind tunnel investigation of control-surface characteristics XXIII : a 0.25-airfoil-chord flap with tab having a chord twice the flap chord on an NACA 0009 airfoil

著录项

• 作者

  Spearman, M Leroy;

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• 作者单位

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• 年度 1945
• 页码 1-59
• 总页数 59
• 原文格式 PDF
• 正文语种 eng
• 中图分类 工业技术;
• 关键词

  CONTROL SURFACES - CHARACTERISTICS; AIRFOILS - NACA 0009 - CHAR & MOMENTS WING FLAPS & TABS; CONTROL SURFACES, BALANCED - HINGE MOMENTS - WIND TUNNEL TESTS; TABS - WIND TUNNEL TESTS; WING FLAPS - DEFLECITON; TABS - DEFLECTION; WING FLAPS, SEALED-GAP; WING FLAPS, BALANCED; WIND TUNNEL TESTS - NACA (6'X4');

  机译：控制表面 - 特征; aIRFOILs - NaCa 0009 - CHaR＆amp;时尚翼展＆amp; TaBs;控制表面，平衡 - 铰链时刻 - 风洞隧道测试; TaBs - 风洞隧道测试;翼襟 - 萎缩; TaBs - DEFLECTION;翼襟翼，密封间隙;翼展，平衡;风洞隧道测试 - NaCa（6'X4'）;