首页> 外国专利> External shape of aerofoil section with profile thickness of 13 per cent, profile curvature of 4 per cent, and moment coefficient with value smaller than 0,004 can be clearly represented by curve with equivalent tabulated values

External shape of aerofoil section with profile thickness of 13 per cent, profile curvature of 4 per cent, and moment coefficient with value smaller than 0,004 can be clearly represented by curve with equivalent tabulated values

机译:翼型截面的外形形状具有13%的轮廓厚度,4%的轮廓曲率和小于0.004的弯矩系数,可以用等效列表值的曲线清楚地表示

摘要

The external shape (2) of an aerofoil section (1) with a profile thickness of 13 per cent, a profile curvature of 4 per cent, and a moment coefficient with a value smaller than 0,004, can be clearly represented by a curve with equivalent tabulated values. The external form of a thin wing root section with a profile thickness of 14 per cent and an inverted profile curvature of 3 per cent can also be clearly represented by a curve with equivalent tabulated values.
机译:翼型截面(1)的外形(2)的轮廓厚度为13%,轮廓曲率为4%,弯矩系数小于0.004,可以用等价曲线清楚地表示列表值。轮廓厚度为14%的薄翼根部段的外部形式和轮廓折曲率为3%的外形也可以通过具有等效列表值的曲线清楚地表示。

著录项

  • 公开/公告号DE202005018086U1

    专利类型

  • 公开/公告日2006-06-01

    原文格式PDF

  • 申请/专利权人 SCHEUERMANN WOLFGANG WERNER;

    申请/专利号DE20052018086U

  • 发明设计人

    申请日2005-11-19

  • 分类号B64C3/14;

  • 国家 DE

  • 入库时间 2022-08-21 21:19:54

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