0
RESEARCH PAPERS

Base Heat Transfer in Two-Dimensional Subsonic Fully Separated Flows

[+] Author and Article Information
John W. Mitchell

Department of Mechanical Engineering, University of Wisconsin, Madison, Wisc.

J. Heat Transfer 93(4), 342-348 (Nov 01, 1971) (7 pages) doi:10.1115/1.3449829 History: Received February 12, 1970; Revised June 04, 1970; Online August 11, 2010

Abstract

An experimental investigation of the heat transfer from the base of a two-dimensional wedge-shaped body to the separated-flow region was conducted in a low-speed wind tunnel. The Stanton number has been determined as a function of Reynolds number for two geometries that are representative of heat-exchanger surfaces. The heat transfer is found to be comparable in magnitude to that for attached flows. An analysis based on the mechanisms of vortex shedding and boundary-layer behavior is developed. The analysis agrees fairly well with the data and indicates the parameters governing base heat transfer.

Copyright © 1971 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