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Unsteady Aerodynamics and Aeroelasticity of Turbomachines pp 259–271Cite as

High Speed Centrifugal Impeller and Diffuser Interaction Near Stall Conditions

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Abstract

Amongst the flow instabilities observed in compressors, stall and surge are taken to be the most disastrous effects upon the performance of turboma-chinery. It is necessary to secure always the surge margin in compressor map when the operation shifts towards the lower mass flow rate.

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References

  • Yamane, T. Fujita, H. Nagashima, T., “An Investigation of Impeller and Diffuser Interaction in a Transonic Centrifugal Compressor”, Unsteady Aerodynamics and Aeroelasticity of Turbomachines, 1995, pp. 499-513.

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  • Yamane, T. Nagashima, T., “Flow Choking and Shock Wave Structure at Diffuser Vanes in a High Speed Centrifugal Impeller”, Proceedings of 12th International Symposium on Air Breathing Engines, Vol.1, 1995, pp. 135–145.

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Author information

Authors and Affiliations

  1. Thermofluid Dynamics Division, National Aerospace Laboratory, 7-44-1 Jindaiji-higashi, Chofu, Tokyo, 182, Japan

    T. Yamane

  2. Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1 Hongo, Bunkyo-ku, Tokyo, 113, Japan

    T. Nagashima

Authors
  1. T. Yamane
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  2. T. Nagashima
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Editor information

Editors and Affiliations

  1. Division of Heat and Power Technology, Royal Institute of Technology, Stockholm, Sweden

    Torsten H. Fransson

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© 1998 Springer Science+Business Media Dordrecht

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Yamane, T., Nagashima, T. (1998). High Speed Centrifugal Impeller and Diffuser Interaction Near Stall Conditions. In: Fransson, T.H. (eds) Unsteady Aerodynamics and Aeroelasticity of Turbomachines. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-5040-8_17

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  • DOI: https://doi.org/10.1007/978-94-011-5040-8_17

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-94-010-6116-2

  • Online ISBN: 978-94-011-5040-8

  • eBook Packages: Springer Book Archive

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