The article describes an algorithm for the inverse calculation of a multi-stage axial compressor using the streamline curvature method. Also, using this method, a four-stage axial compressor with a pressure ratio of 3.2 was designed. In addition, a numerical simulation of the flow in this compressor was performed, the results of the numerical simulation were compared with the design parameters, and an analysis of the reasons for the deviation of the parameters from the design parameters was performed. Recommendations for improving the calculation methodology are given.
Primary Language | English |
---|---|
Subjects | Mechanical Engineering (Other) |
Journal Section | Research Articles |
Authors | |
Publication Date | September 27, 2024 |
Submission Date | June 11, 2024 |
Acceptance Date | June 28, 2024 |
Published in Issue | Year 2024 Volume: 2 Issue: 2 |