0
TECHNICAL BRIEFS

Energy Separation in Steady Separated Wake Flow

[+] Author and Article Information
B. W. van Oudheusden

Department of Aerospace Engineering,  Delft University of Technology, The Netherlands PO Box 5058, 2600 GB Delft, The Netherlands b.w.vanoudheusden@lr.tudelft.nl

J. Fluids Eng 127(3), 611-614 (Feb 22, 2005) (4 pages) doi:10.1115/1.1900141 History: Received May 11, 2004; Revised February 22, 2005

First Page Preview

View Large
First page PDF preview
FIGURES IN THIS ARTICLE
Copyright © 2005 by American Society of Mechanical Engineers
Your Session has timed out. Please sign back in to continue.

References

Figures

Grahic Jump Location
Figure 1

Schematic flow field structure of a supersonic base flow

Grahic Jump Location
Figure 2

Energy separation in compressible base flow (symbols: Numerical data, solid line: Present theory, dashed line: Classic theory)

Grahic Jump Location
Figure 3

Energy separation in steady viscous zero-pressure-gradient flow (Pr=0.7); boundary layer (top), mixing layer (center) and far wake (bottom)

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