0
RESEARCH PAPERS

Heat Transfer for Pulsating Laminar Duct Flow

[+] Author and Article Information
R. Siegel, M. Perlmutter

Lewis Research Center, National Aeronautics and Space Administration (NASA), Cleveland, Ohio

J. Heat Transfer 84(2), 111-122 (May 01, 1962) (12 pages) doi:10.1115/1.3684307 History: Received March 14, 1961

Abstract

Heat-transfer solutions have been obtained for pulsating laminar flow between parallel plates. The pulsations are caused by superposing an oscillating pressure gradient on the steady driving pressure of the flow. Two types of heat-transfer boundary conditions are considered: (a) The channel walls are at constant temperature; or (b) a specified uniform heat flux is transferred at the walls. The heat-transfer behavior is obtained along the entire length of the channel, that is, in both the thermal entrance and fully developed regions. The temperature distributions are two-dimensional, but a slug flow (one-dimensional) assumption is used to simplify the velocity distribution. The results are compared with those obtained using a quasi-steady assumption.

Copyright © 1962 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