A Two-Parameters Theory of Axisymmetric Compressible Flow in Axial Turbomachines

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概要

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• In this paper, a theory of a three-dimensional compressible flow in axial turbomachines with varying boundary shapes is presented, in which the assumption is made that the axial velocity profiles and the specific mass flow profiles are respectively expressible by a single parameter. For these two parameters the flow equations reduce to non-linear ordinary differential equations and can be solved numerically very easily. Comparisons with two more accurate calculations are made to investigate the accuracy of the present theory.

• 一般社団法人日本機械学会の論文

著者

• Kashiwabara Yasushige

  Mechanical Engineering Research Laboratory Hitachi Ltd.

• Kashiwabara Yasushige

  Mechanical Engineering Research Laboratory Of Hitachi Ltd.

関連論文

• A Study on Surge and Rotating Stall in Axial Compressors (A Summary of the Measuremet and Fundamental Analysis Method)
• Experimental and Numerical Analysis of Active Suppression of Centrifugal Compressor Surge by Suction-Side Valve Control
• A Two-Parameters Theory of Axisymmetric Compressible Flow in Axial Turbomachines

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