0
RESEARCH PAPERS

A Quasi-Steady Approach of Wake Effects on Leading Edge Transfer Rates

[+] Author and Article Information
N. T. Van Dresar, R. E. Mayle

Department of Mechanical Engineering, Rensselaer Polytechnic Institute, Troy, NY 12130-3590

J. Turbomach 111(4), 483-490 (Oct 01, 1989) (8 pages) doi:10.1115/1.3262297 History: Received December 01, 1987; Online November 09, 2009

Abstract

Mass transfer experiments are described for a circular cylinder with a steady incident wake flow. Measurements of the velocity, turbulence intensity, intermittency, and integral length scale within the wake are presented together with measurements of the stagnation mass transfer as a function of the cylinder’s position in the wake. Comparison of the results indicates that although the increase in mass transfer occurring along the wake centerline depends on the turbulence intensity, length scale, and possibly other factors, the functional relation with respect to the cylinder’s lateral position in the wake depends on the intermittency and not turbulence level. In addition, a simple quasi-steady theory is developed to account for the unsteady effects caused by the passing of wakes in the incident flow on the stagnation transfer rate at the leading edge of a gas turbine airfoil.

Copyright © 1989 by ASME
Your Session has timed out. Please sign back in to continue.

References

Figures

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