首页> 美国政府科技报告 >The Two-dimensional Subsonic Flow of an Inviscid Fluid about an Aerofoil of Arbitrary Shape Part I. Incompressible Flow about a Symmetrical Aerofoil in a Channel or Free Stream. Part II. Incompressible Flow about an Asymmetric Aerofoil in a Free Stream. Part III. The Influence Factor Method of Calculating Incompressible Flow. Part IV. Compressible Flow.

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The Two-dimensional Subsonic Flow of an Inviscid Fluid about an Aerofoil of Arbitrary Shape Part I. Incompressible Flow about a Symmetrical Aerofoil in a Channel or Free Stream. Part II. Incompressible Flow about an Asymmetric Aerofoil in a Free Stream. Part III. The Influence Factor Method of Calculating Incompressible Flow. Part IV. Compressible Flow.

机译：关于任意形状翼型的Inviscid流体的二维亚音速流动。关于通道或自由流中对称翼型的不可压缩流动。第二部分。关于自由流中不对称翼型的不可压缩流动。第三部分。计算不可压缩流动的影响因素法。第四部分。可压缩流动。

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The paper describes and applies exact methods of calculating the incompressible flow about thick aerofoils of general shape in a free stream, and about symmetrical aerofoils between channel walls. One of these methods is extended to an approximate treatment of subsonic compressible flow by making use of von Karman's transformation.

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L. C. WOODS;
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年度 1953
页码 1-60
总页数 60
原文格式 PDF
正文语种 eng
中图分类工业技术;
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5. Flowfield-Dependent Variation (FDV) method for compressible, incompressible, viscous, and inviscid flow interactions with FDV adaptive mesh refinements and parallel processing. [D] . Heard, Gary Wayne. 2007

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6. The drag on a vibrating aerofoil in incompressible flow. I [O] . Veltkamp, GW 1958

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