Skip to main content
Log in

Investigation of the Vortex Dynamic Mechanism of the Flow Losses on a Transonic Compressor Stator

  • Published:
Journal of Thermal Science Aims and scope Submit manuscript

Abstract

For a transonic axial-flow compressor, the numerical simulations, verified against experimental data, were used to study the inherent correlation between the evolutionary process of the vortex structures and the flow loss in a compressor stator passage during the throttling process. The flow loss was divided accurately and quantitatively, based on the evolutionary process of the vortex structures. According to the position of the singular points of the vortex structures, the influence of the evolution of the vortex structures on the generation and development of the flow loss was analyzed on a microscale scale. Thereafter, this paper provided the vortex dynamic mechanism of the flow loss, which was important to enrich the theoretical system of the flow field in the compressor. The results show that: the flow loss at the top of the stator tip is caused by the low-energy fluid clusters, which are transported and accumulated by the vortices from the endwall; the transport effect of the pressure separation vortex at the upper half-height only migrates the position of the flow losses, but there is new flow loss generated by its shear action to the endwall. The dominant flow loss during the throttling process concentrates upon the closed separation bubble around the middle of the suction side of the stator.

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

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

References

  1. Hu S.Z., Lu X.G., Zhang H.W., et al., Numerical investigation of a high-subsonic axial-flow compressor rotor with non-axisymmetric hub endwall. Journal of Thermal Science, 2010, 19(1): 14–20.

    Article  ADS  Google Scholar 

  2. Wu J.Z., Vortex—the tendon of fluid movement. Chinese Journal of Nature, 1985, 8(7): 490–494. (in Chinese)

    Google Scholar 

  3. Tao D.P., Lu R.F., Zhao X.H., The study of secondary flow in axial compressor cascade. Journal of Beijing Institute of Aeronautics and Astronautics, 1982, 4: 77–90. (in Chinese)

    Google Scholar 

  4. Chen F., Chen M.Z., Jiang H.K., An experimental study of end-wall flow in a compressor cascade. Journal of Engineering Thermophysics, 1988, 9(2): 125–130. (in Chinese)

    Google Scholar 

  5. Tang Y.P., Chen F., Chen M.Z., Experimental investigation on vortical type flow in compressor cascades. Journal of Aerospace Power, 1990, 5(2): 103–112. (in Chinese)

    Google Scholar 

  6. Kang S., Investigation of the three dimensional flow within a compressor cascade with and without tip clearance [D]. Vrije Universiteit Brussel, 1993: I–1–V–44.

    Google Scholar 

  7. Zhang Y.J., Wang H.S., Xu J.Z., et al., Research on topology and vortex structure in diffuser cascades. Science Chinese, Series E: Technological Science, 2009, 39(5): 1016–1025. (in Chinese)

    Google Scholar 

  8. Liu H.P., Chen H.L., Yang X.G., et al., Study of loss mechanism in low speed compressor cascade using dissipation function. Jounal of Aerospace Power, 2011, 26(2): 289–296. (in Chinese)

    Google Scholar 

  9. Tian S.M., Wu Y., Zhang H.D., et al., Energy loss in a low-speed compressor cascade with dissipation function. Acta Aeronautica et Astronautica Sinica, 2015, 36(10): 3249–3262. (in Chinese)

    Google Scholar 

  10. Li X.J., Chu W.L., Zhang H.G., Investigation on relation between secondary flow and loss on a high loaded axial-flow compressor cascade. Journal of Propulsion Technology, 2014, 35(7): 914–925. (in Chinese)

    Google Scholar 

  11. Ling D.J., Wang H., Ma C.Y., Subsonic compressor plane cascade experiment at low Reynolds number. Journal of Aerospace Power, 2013, 28(1): 171–179. (in Chinese)

    Google Scholar 

  12. Zhang H.D., Wu Y., Li Y.H., et al., Investigation of vortex structure and flow loss in a high- speed compressor cascade. Acta Aeronautica ET Astronautica Sinica, 2014, 35 (9): 2438–3450. (in Chinese)

    Google Scholar 

  13. Li Y.H., Ye D.J., et al., Experimental investigation of the three-dimensional flow in an annular compressor cascade at large incidence. Journal of Thermal Science, 1992, 1(1): 3–10.

    Article  ADS  Google Scholar 

  14. Chen S.W., Chen F., Wang K.L., et al., Research on flow separation and vortex structure on a highly loaded annual compressor cascade part 2: cross section in the flow passage[C]// Congress on Thermodynamics and Aerodynamics of Chinese Society of Engineering Thermophysics, 2006, Chongqing, China. (in Chinese)

    Google Scholar 

  15. Liu B.J., Yu X.J., Jiang H.K., Method for analyzing flow losses in turobmachinery by using the measured results of stereoscopic particle image velocimetry. Journal of Aerospace Power, 2009, 24(11): 2551–2557. (in Chinese)

    Google Scholar 

  16. Du H., Yu X.J., Zhang Z.B., et al., Relationship between the flow blockage of tip leakage vortex and its evolutionary procedures inside the rotor passage of a subsonic axial compressor. Journal of Thermal Science, 2013, 22(6): 522–531.

    Article  ADS  Google Scholar 

  17. Ma H.W., Li B.H., Effects of axial non-uniform tip clearances on aerodynamic performance of a transonic axial compressor. Journal of Thermal Science, 2008, 17(4): 331–336.

    Article  ADS  Google Scholar 

  18. Sakata Y., Ohta Y., Coexisting state of surge and rotating stall in a two-stage axial flow compressor using a doublephase-locked averaging technique. Journal of Thermal Science, 2017, 26(1): 38–46.

    Article  ADS  Google Scholar 

  19. Zhang J.X., Li C.Q., A study of the unsteady tip flow field of a transonic compressor. Journal of Thermal Science, 2011, 20(1): 1–5.

    Article  ADS  Google Scholar 

  20. Ma H.W., Jiang H.K., An Experimental Study of Three-Dimensional Characteristics of Turbulent Wakes of Axial Compressor Rotors. Journal of Thermal Science, 2005, 14(1): 15–21.

    Article  ADS  Google Scholar 

  21. Kan X.X., Lu H.W., Zhong J.J., Topological characterization of the vortex structures in the transonic compressor stator during the stalling process. Proceedings of the IMechE, Part G: Journal of Aerospace Engineering, 2016, 230(3): 566–580.

    Google Scholar 

  22. Kan X.X., Lu H.W., Zhong J.J., Study of influence on the rotor wake to the unsteady separation structure on transonic compressor stator. Journal of Engineering Thermophsics, 2015, 36(4): 744–751

    Google Scholar 

  23. Kang S., Wang Z.Q., Application of topo-logical analysis to studying the three-dimensional flow in cascades; part I. topological rules for skin-friction lines and section streamlines. Applied Mathematics and Mechanics, 1990, 11(5): 489–495.

    Google Scholar 

  24. Yamada K., Kikuta H., Iwakiri K.I,, et al., An explanation for flow features of spike-type stall inception in an axial compressor rotor. ASME Journal of Turbomachinery. 2013, 135 (2): 021023-1-11.

    Article  Google Scholar 

  25. Flaszynski P., Doerffer P., Szwaba R., et al., Laminarturbulent transition tripped by step on transonic compressor profile. Journal of Thermal Science, 2018, 27(1): 1–7.

    Article  ADS  Google Scholar 

Download references

Acknowledgment

This work was supported by a project funded by the China Postdoctoral Science Foundation (Grant No. 2017M621268), and the National Natural Science Foundation of China (Grant Nos. 51436002, 51506020, and 51706051).

The authors would like to thank Prof. Jingjun Zhong for the guidance of the vortex structure analysis for the first author's Ph.D. candidate.

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Xiaoxu Kan.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Kan, X., Wang, S., Luo, L. et al. Investigation of the Vortex Dynamic Mechanism of the Flow Losses on a Transonic Compressor Stator. J. Therm. Sci. 28, 51–60 (2019). https://doi.org/10.1007/s11630-018-1029-9

Download citation

  • Received:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s11630-018-1029-9

Keywords

Navigation