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Effects of elevator nose shape, gap, balance, and tabs on the aerodynamic characteristics of a horizontal tail surface

机译：电梯前端形状，间隙，平衡和突片对水平尾翼表面气动特性的影响

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摘要

Results are presented showing the effects of gap, elevator, nose shape, balance, cut-out, and tabs on the aerodynamic characteristics of a horizontal tail surface tested in the NACA full-scale tunnel.

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作者
Goett, Harry J; Reeder, J P;
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年度 1939
页码 1-25
总页数 25
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
HORIZONTAL TAIL SURFACES; ELEVATORS (CONTROL SURFACES); NOSES (FOREBODIES); SHAPES; GAPS; TABS (CONTROL SURFACES); AERODYNAMIC BALANCE; AERODYNAMIC CHARACTERISTICS; FULL SCALE TESTS; WIND TUNNEL TESTS; TORQUE; DEFLECTION; OPENINGS; EXPERIMENTATION; THEORIES; COMPARISON;

机译：水平尾部表面;电梯（控制表面）; NOsEs（FOREBODIEs）; sHapEs; Gaps; TaBs（控制表面）;空气动力学平衡;空气动力学特征;全面测试;风洞隧道测试;扭矩;偏转;开孔;物理实验;理论研究;比较;

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Effects of elevator nose shape, gap, balance, and tabs on the aerodynamic characteristics of a horizontal tail surface

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