A Technique for Calculating Characteristics of Axial Flow Compressor Stage with Blades of Large Relative Length

摘要

The mathematical modeling of gas flow in vane channels of axial compressors in the one-dimensional statement is considered taking into account the radial nonuniformity of flow parameters. Such an approach makes it possible to develop the fast-response algorithms for calculating the characteristics of the axial compressor stage when the working body parameters change at inlet and turn of inlet guide vanes.