Development of a Streamline Method

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Abstract
The research investigated and developed a novel streamline method for the computation of steady state compressible flows in ducts and axial compressors. The method is based on the description of a streamline in terms of axial position and two parameters. A coupled pair of second order differential equation are developed and solved by a relaxing process in the subsonic case, and by downstream marching in the supersonic case. Computational Aerodynamics, Axial flows.

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