Skip to main content

Influence of Endwall Clearance on HSV and Passage Flow Between Two Turbine Cascade Blades

  • Conference paper
  • First Online:
Fluid Mechanics and Fluid Power – Contemporary Research

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

  • 3101 Accesses

Abstract

Horseshoe vortex is formed at the junction of an object immersed in fluid-flow and endwall as a result of three-dimensional boundary layer separation. When a boundary layer flow (either laminar or turbulent) encounters any obstacle projecting from the surface, some distance upstream of the obstacle the boundary layer separates as a result of the adverse pressure gradient, and rolls up to form three-dimensional complex vortices. Generally horseshoe vortex is observed near the endwall region and also forms near the tip endwall clearances. The passage flow is characterized by boundary layer effects, secondary flows generated by the pressure gradients, leading edge horseshoe vortex formation. The vortices form the characteristics of horseshoe shaped vortex, with legs of the vortices extending to downstream, on both sides of the blade. The numerical study was carried out for two turbine blades, considering the effect with and without endwall tip clearances from 0 to 5 % of span of the airfoil. The flow without tip clearance (c = 0 mm), will have maximum influence of the horseshoe vortex structure formation, because of strong pressure gradient observed near to the region to the blade leading edge. This affects the secondary flows in the endwall region, which implies more losses. And for the flow with higher clearances (c = 5 mm), it is observed that the horseshoe vortex formation in the leading edge of the blade is very weak, because of reduced adverse pressure gradient. The numerical simulation has been carried out for two turbine blades to study HSV structure and the interference effects on the blade flow characteristics. Additionally, the passage flow between the two turbine blades with and without endwall clearance effect is studied. Results of the numerical simulation of horseshoe vortex formation and effect of endwall clearances on the structures are presented. The velocity and static pressure are plotted and studied.

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 259.00
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 329.99
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

Bibliography

  1. Baker, C.J.: The laminar Horseshoe vortex. J. Fluid Mech. 95, 347–367 (1979)

    Google Scholar 

  2. Ishii, J., Honami, S.: A three-dimensional turbulent detached flow with a Horseshoe vortex. J. Eng. Gas Turbines Power 108, 125–130 (1986)

    Google Scholar 

  3. Moore, J., Tilton, J.S.: Tip leakage flow in a linear turbine cascade. J. Turbo Mach. 110, 18–26 (1988)

    Google Scholar 

  4. Kang, K.J., Kim, T., Song, S.J.: Strengths of horseshoe vortices around a circular cylinder with an upstream cavity. J. Mech. Sci. Technol. 23, 1773–1778 (2009)

    Google Scholar 

  5. Tsujita, Hoshio, Yamamoto, Atsumasa: Influences of incidence angle on 2D-flow and secondary flow structure in ultra-highly loaded turbine cascade. J. Therm. Sci. 23, 13–21 (2014)

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to V. Vikram .

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2017 Springer India

About this paper

Cite this paper

Vikram, V., Gowda, B.H.L., Prasad, B.B.S.S.S. (2017). Influence of Endwall Clearance on HSV and Passage Flow Between Two Turbine Cascade Blades. In: Saha, A., Das, D., Srivastava, R., Panigrahi, P., Muralidhar, K. (eds) Fluid Mechanics and Fluid Power – Contemporary Research. Lecture Notes in Mechanical Engineering. Springer, New Delhi. https://doi.org/10.1007/978-81-322-2743-4_78

Download citation

  • DOI: https://doi.org/10.1007/978-81-322-2743-4_78

  • Published:

  • Publisher Name: Springer, New Delhi

  • Print ISBN: 978-81-322-2741-0

  • Online ISBN: 978-81-322-2743-4

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics