Skip to main content

Diagnosis and Analysis of Interstage Flow Field in a High Load Compressor

  • Conference paper
  • First Online:
Proceedings of the 6th China Aeronautical Science and Technology Conference (CASTC 2023)

Part of the book series: Lecture Notes in Mechanical Engineering ((LNME))

Included in the following conference series:

  • 207 Accesses

Abstract

This article conducted flow field refinement tests on a high load compressor using steady-state five hole probes, high-frequency dynamic probes, and blade probes, and obtained detailed inter stage flow field characteristics such as total pressure, total temperature, and Mach number. The results showed that by analyzing and comparing the flow field parameters of the compressor’s overall performance and inter stage performance tests with CFD design performance, the main characteristics that affect compressor performance can be effectively obtained, Obtain the flow field performance of the blade near the end wall and upstream and downstream blades, among which the steady-state five hole probe and dynamic single hole probe effectively overcome the problem of limited conventional measurement space for the compressor; The blade probe obtained detailed flow field distributions of performance parameters along the radial and circumferential directions of the 1–3 stage rotor, providing experimental data support for compressor flow field diagnosis and performance optimization.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 189.00
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 249.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

References

  1. Peng, Z., Liu, G.: Principles of aviation gas turbine, pp. 66–68. National Defense Industry Press, Beijing (2000). (in Chinese)

    Google Scholar 

  2. Fei, Y., Liu, Y., Lu, L.: Modification of realizable κ-ε model for tip-leakage flow in an axial compressor rotor. J. Eng. Thermophys. 40(3), 505–512 (2019)

    Google Scholar 

  3. Chen, M., Liu, B.: Fan/compressor aero design trend and challenge on the development of high bypass ratio turbofan. J. Aerosp. Power 23(6), 961–975 (2008)

    Google Scholar 

  4. David, J.: Advanced experimental techniques in turbomachinery, pp. 22–25. Concepts Eti., Norwich (1986)

    Google Scholar 

  5. Liu, Q., Zhou, X.: Numerical analysis of three-dimensional viscous flow through multistage fan and compressors. J. Eng. Thermophys. 22(4), 52–55 (2001). (in Chinese)

    Google Scholar 

  6. Sun, H., Ye, N., Wang, J., et al.: Effect of tip clearance on axial compressor performance and flow field. Aeroengine 40(3), 1–7 (2014). (in Chinese)

    Google Scholar 

  7. Jiang, H., et al.: The experimental device and dynamic measurement technology of large-size axial compressor flowing in the rotor were studied. J. Aerodyn. 1 (1992)

    Google Scholar 

  8. Denton, J.D.: Some limitations of turbomachinery CFD. ASME Turbo Expo Power for Land Sea & Air, Glasgow, No. GT2010-22540, pp. 735–745 (2010)

    Google Scholar 

  9. Ye, D., Yuan, X.: Development of flow field diagnostics. In: Compilation of Special Reports of the Symposium on Development Strategy of Aerothermodynamics, pp. 126–130 (1989)

    Google Scholar 

  10. Roberts, W.B., Serovy, G.K., Sandercock, D.M.: Modeling the 3-D Flow Effects on Deviation Angle for Axial Compressor Middle Stages. ASME paper85-GT-189 (1985)

    Google Scholar 

  11. Li, J., Ma, H., He, X.: Method of measuring 3-D unsteady flow at exits of transonic compressor rotor passages using a two-hole tip-wedge pressure probe. J. Aerosp. Power 27(10), 2262–2268 (2012)

    Google Scholar 

  12. Ma, H., Wei, W., Zhang, L., Guan, H.: Analysis of measured unsteady flow field using a quasi fast response pressure probe. Aeroengine 42(2), 67–72 (2016)

    Google Scholar 

  13. Zhao, Q., Duan, L., Shen, P.: HB7115-94 compressor aerodynamic performance test, pp. 2–7. China Aviation Industry Corporation, Beijing (1995). (in Chinese)

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Anni Wang .

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2024 Chinese Society of Aeronautics and Astronautics

About this paper

Check for updates. Verify currency and authenticity via CrossMark

Cite this paper

Wang, A., Zhang, Z., Chen, Y., Wang, X. (2024). Diagnosis and Analysis of Interstage Flow Field in a High Load Compressor. In: Proceedings of the 6th China Aeronautical Science and Technology Conference. CASTC 2023. Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-99-8867-9_14

Download citation

  • DOI: https://doi.org/10.1007/978-981-99-8867-9_14

  • Published:

  • Publisher Name: Springer, Singapore

  • Print ISBN: 978-981-99-8866-2

  • Online ISBN: 978-981-99-8867-9

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics