Boundary-Layer Transition Regions on Turbine Blade Suction Surfaces PUBLIC ACCESS

[+] Author Affiliations
G. Roberts

Polytechnic of Wales, Treforest, Pontypridd, Mid Glamorgan, Wales

A. Brown

Royal Military College of Science, Shrivenham, Swindon, Wilts, England

Paper No. 84-GT-284, pp. V004T09A022; 10 pages
  • ASME 1984 International Gas Turbine Conference and Exhibit
  • Volume 4: Heat Transfer; Electric Power
  • Amsterdam, The Netherlands, June 4–7, 1984
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7949-8
  • Copyright © 1984 by ASME


This paper describes the results of an experimental investigation into extended boundary-layer transition regions on suction surfaces of four sets of turbine blades in a cascade rig. A transition model is proposed which is tested with some success in a modified version of STAN5, a boundary-layer computer programme.

Copyright © 1984 by ASME
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