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Flow separation control by using bowed blade in highly loaded turbine cascades

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Abstract

Due to the serious flow separations and centralized vortices, there are high secondary losses in highly loaded turbines. It is imperative to find measures to control the flow separation and vortices hence improve the turbine performance. This paper reports our recent progress on flow separation and vortices control in highly loaded turbine cascades by using bowed blades. Two sets of highly loaded turbine cascades with the turning angles of 113° and 160°, and each with 7 bowed blade angles 0° (straight), ±10°, ±20° and ±30° were experimentally investigated. Both internal flow field measurement and flow visualization on the blade surfaces were conducted, and the effects of blade bowing on the flow topology, distribution of vorticity and the flow energy loss were discussed. The results show that, for the cascade with the turning angle of 113°, the appropriately positive bow angle could reduce the flow energy loss; whereas for the cascade with the turning angle of 160°, the well selected negative bow angle can give the better aerodynamic performance.

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References

  1. Moustapha S H, Paron G J, Wade J H T. Secondary flow in cascades of highly loaded turbine blades. ASME J Eng Gas Turb Power, 1985, 105(10): 1031–1038

    Article  Google Scholar 

  2. Moustapha S H, Okapuu U, Williamson R G. Influence of rotor blade aerodynamic loading on the performance of a highly loaded turbine Stage. ASME J Turbomach, 1987, 109(1): 155–162

    Article  Google Scholar 

  3. Lisa W G, Frank W H. Advancement of turbine aerodynamic design techniques. ASME Paper, 1993, 93-GT-370

  4. Yamamoto A, Matsunuma H, Outa E. Three-dimensional flows and losses in an ultra-highly loaded turbine. In: Proceedings of ISROMAC-7. Hawaii: Bird Rock Publishing House, 1998

    Google Scholar 

  5. Yamamoto A. Some current studies on turbine aerodynamics at NAL. In: Proceedings of Colloquium on Turbomachinery. Seoul: Seoul National University Press, 1996

    Google Scholar 

  6. Yamamoto A, Usui H, Tan C, et al. Research on ultra-highly loaded turbine. In: 2nd Japan ESPR Meeting. Tokyo: Japan Aerospace Exploration Agency, 2004

    Google Scholar 

  7. Wang Z, Lai S, Xu W. Aerodynamic calculation of turbine stator cascades with curvilinear leaned blades and some experimental results. In: Symposium Paper of 5th ISABE. India: American Institute of Aeronautics and Astronautics, 1981

    Google Scholar 

  8. Han W, Wang Z, Tan C, et al. Effects of leaning and curving of blades with high turning angles on the aerodynamic characteristics of turbine rectangular cascades. ASME J Turbomach, 1994, 116(3): 417–424

    Article  Google Scholar 

  9. Tan C, Yamamoto A, Mizuki S, et al. Influences of blade curving on flow fields of a typical stator cascade. AIAA J, 2003, 41(10): 1967–1972

    Article  Google Scholar 

  10. Tan C, Yamamoto A, Chen H. Flowfield and aerodynamic performance of a turbine stator cascade with bowed blades. AIAA J, 2004, 42(10): 2170–2171

    Article  Google Scholar 

Download references

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Correspondence to HuaLiang Zhang.

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Supported by the National Natural Science Foundation of China (Grant No. 10577019)

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Tan, C., Zhang, H., Chen, H. et al. Flow separation control by using bowed blade in highly loaded turbine cascades. Sci. China Ser. E-Technol. Sci. 52, 1471–1477 (2009). https://doi.org/10.1007/s11431-009-0176-3

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  • DOI: https://doi.org/10.1007/s11431-009-0176-3

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