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Effects of aerodynamic unsteadiness in axial turbomachines

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VKI LS 2005-03, Effects of aerodynamic unsteadiness in axial turbomachines

Effects of aerodynamic unsteadiness in axial turbomachines

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Effects of aerodynamic unsteadiness in axial turbomachines
April 25 - 29, 2005; R. Dénos & G. Paniagua
Table of contents
  • TAN, C.S. – MIT Gas Turbine Laboratory, USA
    Unsteady flows in compressors
  • DÉNOS, R. & PANIAGUA, G. – von Karman Institute for Fluid Dynamics, Belgium
    Unsteady flows in turbines: generalities
    Unsteady flows in transonic HP turbines
  • HODSON, H.P.1 & HOWELL, R.J.21Whittle Laboratory & 2Siemens, United Kingdom
    The role of transition in high lift low pressure turbines
  • NÜRNBERGER, D. – DLR, Germany Aerospace Center, Germany
    Numerical methods and models for unsteady flows in turbomachines
  • EULITZ, F. & SCHMITT, S. – Siemens Power Generation, Germany
    Numerical methods: application to turbine flow
  • FRANSSON, T.H. – KTH Stockholm, Sweden
    Overview: aeroelasticity in axial-flow turbomachines
    Basic introduction to aeroelasticity
    Aeroelastic facilities / aerodynamics measurements
    Dynamic aeroelasticity / Important parameters / Time-dependent aerodynamic nomenclature
  • SEINTURIER, E. – Turboméca, France
    Forced response computation for bladed disks – Industrial practices and advanced methods
    Forced response computation for bladed disks – Application to research cases and industrial problems
  • ROGER, M. – Ecole Centrale de Lyon, France
    Aeroacoustics

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Manufacturer von Karman Institute for Fluid Dynamics

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