Skip to main content
Log in

Topology and vortex structures of a curving turbine cascade with tip clearance (I)—Experimental model and topological flow patterns on both endwalls and blade surfaces

  • Published:
Applied Mathematics and Mechanics Aims and scope Submit manuscript

Abstract

By means of ink trace visualization of the flows in conventional straight, positively curved and negatively curved cascades with tip clearance, and measurement of the aerodynamic parameters in the transverse section, and by appling topology theory, the structures on both endwalls and blade surfaces were analyzed. Compared with conventional straight cascade, blade positive curving eliminates the separation line of the upper passage vortex and leads the secondary vortex to change from close separation to open separation, while blade negative curving effects merely the positions of singular points and the intensities and scales of vortex.

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. QUAN Sheng-lin. Experimental research of the influence on clearance flow by blade curving[D]. Harbin: Harbin Institute of Technology, 1997. (in Chinese)

    Google Scholar 

  2. WANG Zhong-qi, HAN Wang-jin. The influence of blade negative curving on the endwall and blade surface flows[R]. ASME Paper 95-GT-441, 1995.

  3. HAN Wan-jin, WANG Zhong-qi. Effect of blade curving on streamwise vortex system in cascade outlet field[A]. In: CHEN Nan-xing, JIANG Hong-de Eds.Proc 1 st Int Symp Exper Compal Aerothermodyn Internal Flows[C]. Beijing: Word Publishing Corporation, 1990,321–325.

    Google Scholar 

  4. Yamamoto A: Endwall flow/loss mechanisms in a linear turbine cascade with blade tip clearance [J].Trans ASME J Turbomachinery, 1989,111:264–275.

    Article  Google Scholar 

  5. Lighthill M J. Introduction: boundary layer theory[A]. In: Rosenhead Ed.Laminer Boundary Layers[C]. Oxford: Oxford Univ Press, 1963,46–113.

    Google Scholar 

  6. KANG Shun. Investigation on the three-dimensional flow within a compressor cascade with and without tip clearance[D]. Ph D Thesis. Brussel: Vrije Universiteit Brussel, 1993.

    Google Scholar 

  7. XIA Xue-qian, DENG Xue-ying. Engineering Separation Flow Dynamics[M]. Beijing: Publishing House of Beijing University of Aviation and Spaceflight, 1991. (in Chinese)

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Additional information

Communicated by DAI Shi-qiang

Foundation items: 973 Project of China; the Doctoral Foundation of Education Ministry of China (EDAF24403003)

Biography: YANG Qing-hai (1969−)

Rights and permissions

Reprints and permissions

About this article

Cite this article

Qing-hai, Y., Hong-yan, H. & Wan-jin, H. Topology and vortex structures of a curving turbine cascade with tip clearance (I)—Experimental model and topological flow patterns on both endwalls and blade surfaces. Appl Math Mech 23, 948–957 (2002). https://doi.org/10.1007/BF02437800

Download citation

  • Received:

  • Revised:

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF02437800

Key words

CLC number

Navigation