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Two-dimensional wind-tunnel investigation of a 10.7-percent-thick symmetrical tail section with a 0.40 airfoil-chord control surface and a 0.20 control-surface-chord tab

机译：二维风洞研究10.7％厚的对称尾部，带有0.40翼型弦控制面和0.20控制表面弦杆

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Braslow, Albert L;
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年度 1947
页码 1-39
总页数 39
原文格式 PDF
正文语种 eng
中图分类工业技术;
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入库时间 2022-08-29 11:20:22

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8. Two-Dimensional Wind-Tunnel Investigation of a 10.7-Percent-Thick Symmetrical Tail Section with a 0.40 Airfoil-Chord Control Surface and a 0.20 Control-Surface-Chord Tab [R] . Braslow, A. L. 1947

机译：用0.40翼型和弦控制表面的10.7％的厚对称尾段二维风洞调查和0.20操纵面和弦标签

Two-dimensional wind-tunnel investigation of a 10.7-percent-thick symmetrical tail section with a 0.40 airfoil-chord control surface and a 0.20 control-surface-chord tab

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