An Approximate Theory of Airfoil Cascade in Subsonic Flow

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概要

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• This paper deals with an approximate theory of airfoil cascades in subsonic flow. The theory was developed by the so-called "Interference Method" and Prandtl-Glauert's approximate theory of airfoil. The calculated results of some airfoil cascades coincide well with the ones calculated by the "Hodograph Method". The Inverse Problem is also discussed in this paper.

• 一般社団法人日本機械学会の論文

著者

• Ishida Shuji

  Hitachi Ltd.

• Kamimoto Goro

  Aeronautical Engineering Kyoto University

• Akamatsu Teruaki

  Mechanical Engineering Kyoto University

• KAMIMOTO Goro

  Aeronautical Engineering, Kyoto University

関連論文

• An Approximate Theory of Airfoil Cascade in Subsonic Flow
• Theory of Centrifugal Type Impeller with Vanes of Arbitrary Form

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