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Aero-Thermo-Mechanical Design Analysis

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  • M., TAYLOR - Rolls-Royce Aerospace, UK: HP axial flow turbine aerodynamic design
  • G., PANIAGUA & R., DÉNOS - von Karman Institute for Fluid Dynamics, Belgium: Unsteadyness in HP turbines
  • H.P., HODSON & R.J., HOWELL - Whittle Laboratory, UK & Sheffield University, UK: The role of transition in high lift low pressure turbines Part 1 – Part 2
  • C.S., TAN – MIT, USA: Unsteady flows in compressors
  • E., SEINTURIER – Turbomeca, France: Forced response computation for bladed disks industrial practices and advanced methods Part 1 – ¨Part 2
  • R.S., BUNKER - GE Global Research, NY, USA: Blade tip cooling requirements and design Part 1
  • R.S., BUNKER - GE Global Research, NY, USA: Blade tip cooling requirements and design Part 2

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Manufacturer von Karman Institute for Fluid Dynamics

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