Araştırma Makalesi
BibTex RIS Kaynak Göster
Yıl 2024, Cilt: 2 Sayı: 2, 106 - 120, 27.09.2024

Öz

Kaynakça

  • 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

Yıl 2024, Cilt: 2 Sayı: 2, 106 - 120, 27.09.2024

Öz

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.

Kaynakça

  • 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.
Toplam 9 adet kaynakça vardır.

Ayrıntılar

Birincil Dil İngilizce
Konular Makine Mühendisliği (Diğer)
Bölüm Research Articles
Yazarlar

Hadi Genceli

Rafis Mukhamediarov Bu kişi benim

Yayımlanma Tarihi 27 Eylül 2024
Gönderilme Tarihi 11 Haziran 2024
Kabul Tarihi 28 Haziran 2024
Yayımlandığı Sayı Yıl 2024 Cilt: 2 Sayı: 2

Kaynak Göster

IEEE H. Genceli ve R. Mukhamediarov, “Implementing the Streamline Curvature Method For Preliminary Design of Multi-Stage Axial Compressors”, IJONFEST, c. 2, sy. 2, ss. 106–120, 2024.