首页> 美国政府科技报告 >Aerodynamic Characteristics in the Approach, Superfine and Negative Pitch Ranges of Two Four-Bladed Propellers with N.A.C.A. Series 16 Blade Sections a Report of Tests carried out Jointly by the Technical Staffs of de Havilland Propellers, Limited, and Rotol, Limited.
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Aerodynamic Characteristics in the Approach, Superfine and Negative Pitch Ranges of Two Four-Bladed Propellers with N.A.C.A. Series 16 Blade Sections a Report of Tests carried out Jointly by the Technical Staffs of de Havilland Propellers, Limited, and Rotol, Limited.

机译:N.a.C.a.两个四叶螺旋桨接近,超细和负螺距的气动特性16系列叶片部分由de Havilland propellers,Limited和Rotol,Limited的技术人员共同执行的测试报告。

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摘要

Tests were conducted on two similar full-scale propellers in the 24-ft Wind Tunnel at the Royal Aircraft Establishment by representatives of Rotol, Ltd. and de Havilland Propellers, Ltd. to measure the aerodynamic characteristics over a blade-angle range of — 20 deg to + 40 deg, measured at the 0 . 7 radius, and over a range of advance ratio of 0.1 to 2.4.

著录项

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  • 作者单位
  • 年度 1959
  • 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

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