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Effects of aerodynamic unsteadiness in axial Turbomachines article pay-per-view 25€/article

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Effects of aerodynamic unsteadiness in axial Turbomachine

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  • C.S., TAN – MIT Gas Turbine Laboratory, USA: Unsteady flows in compressors
  • R., DÉNOS & G., PANIAGUA – von Karman Institute for Fluid Dynamics, Belgium: Unsteady flows in turbines: generalities
  • R., DÉNOS & G., PANIAGUA – von Karman Institute for Fluid Dynamics, Belgium: Unsteady flows in transonic HP turbines
  • H.P., HODSON 1 & R.J., HOWELL 2 – 1 Whittle Laboratory & Siemens, 2 United Kingdom: The role of transition in high lift low pressure turbines
  • D., NÜRNBERGER – DLR, Germany Aerospace Center, Germany: Numerical methods and models for unsteady flows in turbomachines
  • E., SEINTURIER – Turboméca, France: Forced response computation for bladed disks – Industrial practices and advanced methods
  • E., SEINTURIER – Turboméca, France: Forced response computation for bladed disks – Application to research cases and industrial problems
  • M., ROGER – Ecole Centrale de Lyon, France: Aeroacoustics

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