Welcome to the von Karman Institute for Fluid Dynamics Store

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

Be the first to review this product

Availability: In stock


Quick Overview

Boundary layers in turbomachines

Article pay-per-view

Double click on above image to view full picture

Zoom Out
Zoom In

More Views

  • Article pay-per-view

* Required Fields



  • 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

Additional Information

Manufacturer von Karman Institute for Fluid Dynamics

Product Tags

Use spaces to separate tags. Use single quotes (') for phrases.