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Effect of Mach number on position error as applied to a pitot-static tube located 0.55 chord ahead of an airplane wing

机译：马赫数对位置误差的影响应用于位于飞机机翼前方0.55弦的皮托静压管

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Lindsey, W F;
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年度 1944
页码 1-5
总页数 5
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
INSTRUMENTS - PITOT-STATIC TUBES - POSITION; MACH NUMBER; AIRFOILS - THICKNESS; AIRFOILS - CHARACTERISTICS; EFFECT OF COMPRESSIBILITY; AIRFOILS - NACA 16-106; AIRFOILS - NACA 16-215; AIRFOILS - NACA 16-130; WIND TUNNELS - NACA - HIGH-SPEED (2 FEET) (AMER ); WIND TUNNEL TESTS - NACA - HIGH-SPEED (2 FEET);

机译：仪器 - pITOT-sTaTIC TUBEs - 位置;马赫数;翼型 - 厚度;翼型 - 特征;可压缩性的影响; aIRFOILs - NaCa 16-106; aIRFOILs - NaCa 16-215; aIRFOILs - NaCa 16-130;风洞隧道 - NaCa - 高速（2英尺）（美国）;风洞隧道测试 - NaCa - 高速（2英尺）;

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7. Effect of Mach Number on Position Error as Applied to a Pitot-Static Tube Located 0.55 Chord Ahead of an Airplane Wing. [R] . Lindsey, W. F. 1944

机译：马赫数对位置误差的应用效果的皮托静压管位于0.55和弦未来的飞机机翼。

Effect of Mach number on position error as applied to a pitot-static tube located 0.55 chord ahead of an airplane wing

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