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Year 2024, Volume: 2 Issue: 2, 106 - 120, 27.09.2024

Abstract

References

  • Tao, L., Yadong, W., & Hua, O. (2020). Performance Prediction of Transonic Axial Compressors Using Improved Streamline Curvature Approach. Fluid Dynamics, 55(1), 121–132.
  • Jansen, W., & Moffatt, W. C. (1967). The off-design analysis of axial-flow compressors.
  • Aungier, R. H. (2003). Axial-flow compressors. American Society of Mechanical Engineers, New York.
  • Cumpsty, N. A. (1989). Compressor aerodynamics. Longman Scientific & Technical.
  • Banjac, Milan & Petrovic, Milan. (2018). Development of Method and Computer Program for Multistage Axial Compressor Design: Part II — Two-Dimensional Design and Validation Using CFD. V02CT42A008. 10.1115/GT2018-75412.
  • Lieblein, S., 1959. “Loss and Stall Analysis of Compressor Cascades”. ASME Journal of Basic Engineering, 81, pp. 387–400.
  • Schobeiri, M. (2005). Turbomachinery flow physics and dynamic performance (p. 153). Berlin: Springer. [8] Bogdonoff, S. M. (1948). NACA Cascade Data for the Blade Design of High-Performance Axial-Flow Compressors. Journal of the Aeronautical Sciences, 15(2), 89-95.
  • ANSYS, 2010. ANSYS CFX-Solver Theory Guide. ANSYS Inc, Canonsburg.
  • Statrtsev, A.N. (2021). Аэродинамическое проектирование осевого компрессора [Design of an axial compressor aerodynamics]. Aircraft Engines 3(12), 19-34.

Implementing the Streamline Curvature Method For Preliminary Design of Multi-Stage Axial Compressors

Year 2024, Volume: 2 Issue: 2, 106 - 120, 27.09.2024

Abstract

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.

References

  • Tao, L., Yadong, W., & Hua, O. (2020). Performance Prediction of Transonic Axial Compressors Using Improved Streamline Curvature Approach. Fluid Dynamics, 55(1), 121–132.
  • Jansen, W., & Moffatt, W. C. (1967). The off-design analysis of axial-flow compressors.
  • Aungier, R. H. (2003). Axial-flow compressors. American Society of Mechanical Engineers, New York.
  • Cumpsty, N. A. (1989). Compressor aerodynamics. Longman Scientific & Technical.
  • Banjac, Milan & Petrovic, Milan. (2018). Development of Method and Computer Program for Multistage Axial Compressor Design: Part II — Two-Dimensional Design and Validation Using CFD. V02CT42A008. 10.1115/GT2018-75412.
  • Lieblein, S., 1959. “Loss and Stall Analysis of Compressor Cascades”. ASME Journal of Basic Engineering, 81, pp. 387–400.
  • Schobeiri, M. (2005). Turbomachinery flow physics and dynamic performance (p. 153). Berlin: Springer. [8] Bogdonoff, S. M. (1948). NACA Cascade Data for the Blade Design of High-Performance Axial-Flow Compressors. Journal of the Aeronautical Sciences, 15(2), 89-95.
  • ANSYS, 2010. ANSYS CFX-Solver Theory Guide. ANSYS Inc, Canonsburg.
  • Statrtsev, A.N. (2021). Аэродинамическое проектирование осевого компрессора [Design of an axial compressor aerodynamics]. Aircraft Engines 3(12), 19-34.
There are 9 citations in total.

Details

Primary Language English
Subjects Mechanical Engineering (Other)
Journal Section Research Articles
Authors

Hadi Genceli

Rafis Mukhamediarov This is me

Publication Date September 27, 2024
Submission Date June 11, 2024
Acceptance Date June 28, 2024
Published in Issue Year 2024 Volume: 2 Issue: 2

Cite

IEEE H. Genceli and R. Mukhamediarov, “Implementing the Streamline Curvature Method For Preliminary Design of Multi-Stage Axial Compressors”, IJONFEST, vol. 2, no. 2, pp. 106–120, 2024.