0
TECHNICAL PAPERS

An Experimental Study of the Effect of Wake Passing on Turbine Blade Film Cooling

[+] Author and Article Information
James D. Heidmann, Barbara L. Lucci

NASA Glenn Research Center, Cleveland, OH

Eli Reshotko

Case Western Reserve University, Department of Mechanical and Aerospace Engineering, Cleveland, OH

J. Turbomach 123(2), 214-221 (Feb 01, 1997) (8 pages) doi:10.1115/1.1354621 History: Received February 01, 1997
Copyright © 2001 by ASME
Your Session has timed out. Please sign back in to continue.

References

Figures

Grahic Jump Location
Rotor-wake facility schematic
Grahic Jump Location
Film hole and gauge arrangement
Grahic Jump Location
Time- and span-average film effectiveness
Grahic Jump Location
Steady span-average film effectiveness, M=1.0
Grahic Jump Location
Steady span-average Nusselt number, M=1.0
Grahic Jump Location
Local film effectiveness, CO2,M=1.0,x/d=−8.0
Grahic Jump Location
Span-average film effectiveness, CO2,M=1.0,St=0

Tables

Errata

Discussions

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In