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INFLUENCE OF A VIBRATION AMPLITUDE DISTRIBUTION ON THE AERODYNAMIC STABILITY OF A LOW-PRESSURE TURBINE SECTORED VANE

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UNSTEADY AERODYNAMICS, AEROACOUSTICS AND AEROELASTICITY OF TURBOMACHINES

Abstract

A parametrical analysis summarizing the effect of the reduced frequency and sector mode shape is carried out for a low-pressure sectored vane cascade for different vibration amplitude distributions between the airfoils in sector as well as the numbers of the airfoils in sector. Critical reduced frequency maps are provided for torsion- and bending-dominated sector mode shapes.

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References

  1. Whitehead, D. S., and Evans, D. H., 1992, “Flutter of grouped turbine blades”, 92-GT-227, ASME Gas Turbine and Aeroengine Congress and Exposition, Cologne, Germany.

    Google Scholar 

  2. Kahl, G., 1995, “Application of the time linearized Euler method to flutter and forced response calculations”, ASME paper 95-GT-123.

    Google Scholar 

  3. Chernysheva, O. V., Fransson, T. H., Kielb, R., E., and Barter, J., 2003, “Effect of sector mode shape variation on the aerodynamic stability of a low-pressure turbine sectored vane”, GT2003–38632, ASME/IGTI Turbo Expo, Atlanta, Georgia, USA.

    Google Scholar 

  4. Panovsky, J., and Kielb, R., E., 1998, “A design method to prevent low-pressure turbine blade flutter”, 98-GT-575, ASME Gas Turbine Conference and Exhibition, Stockholm, Sweden.

    Google Scholar 

  5. Tchernysheva, O. V., Fransson, T. H., Kielb, R., E., and Barter, J., 2001, “Comparative analysis of blade mode shape influence on flutter of two-dimensional turbine blades”, ISABE-2001-1243, XVISOABE Conference, Bangalore, India.

    Google Scholar 

  6. Lane, F., 1956, “System mode shapes in the flutter of compressor blade rows”, Journal of the Aeronautical Science, Jan., pp. 54–66.

    Google Scholar 

  7. Holmes, D., G., and, Chuang, H.A., 1991, “2D linearized harmonic Euler flow analysis for flutter and forced response”, Unsteady Aerodynamics Aeroacoustics and Aeroelasticity of Turbomachines and Propellers, Springer Verlag, New York, pp. 213–230.

    Google Scholar 

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© 2006 Springer

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Chernysheva, O.V., Fransson, T.H., Kielb, R.E., Barter, J. (2006). INFLUENCE OF A VIBRATION AMPLITUDE DISTRIBUTION ON THE AERODYNAMIC STABILITY OF A LOW-PRESSURE TURBINE SECTORED VANE. In: Hall, K.C., Kielb, R.E., Thomas, J.P. (eds) UNSTEADY AERODYNAMICS, AEROACOUSTICS AND AEROELASTICITY OF TURBOMACHINES. Springer, Dordrecht. https://doi.org/10.1007/1-4020-4605-7_2

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  • DOI: https://doi.org/10.1007/1-4020-4605-7_2

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-1-4020-4267-6

  • Online ISBN: 978-1-4020-4605-6

  • eBook Packages: EngineeringEngineering (R0)

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