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Boundary layers in turbomachines article pay-per-view VKI LS 1991-06

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Boundary layers in turbomachines

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  • R.E., MAYLE -RENSSELAER POLYTECHNIC INSTITUTE, USA: Fundamental aspects of boundary layers and transition in turbomachines
  • T., SCHRÖDER -MTU-MOTOREN & TURBINEN UNION, MUNICH, GERMANY: Investigations of blade row interaction and boundary layer transition phenomena
    in a multistage aeroengine flow-pressure turbine by measurements with hot film
    probes and surface-mounted hot film gauges
  • R., NARASIMHA -NATIONAL AERONAUTICAL LAB. BANGALORE, INDIA: The dynamics of the transition zone and its modeling
  • H.P., HODSON -CAMBRIDGE u., WHITTLE LAB., UK: Aspects of unsteady blade-surface boundary layers and transition in axial turbomachines
  • R.I., CRANE -IMPERIAL COLLEGE, LONDON, UK: Boundary layers and transition on concave surfaces
  • G., SCHEUERER -ADVANCED SCIENTIFIC COMPUTING GMBH, GERMANY: Numerical prediction of boundary layers and transitional flows
  • J., COSTA & T. Arts -VON KARMAN INSTITUTE, BELGIUM: Boundary layer transition under the presence of discrete frequencies in the freestream turbulence spectrum

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