0
TECHNICAL BRIEFS

Periodic Flow Between Low Aspect Ratio Parallel Jets

[+] Author and Article Information
Elgin A. Anderson, Deryl O. Snyder, Jonathan Christensen

Mechanical and Aerospace Engineering Department, Utah State University, Logan, UT 84322

J. Fluids Eng 125(2), 389-392 (Mar 27, 2003) (4 pages) doi:10.1115/1.1537257 History: Received June 20, 2002; Revised October 22, 2002; Online March 27, 2003
Copyright © 2003 by ASME
Your Session has timed out. Please sign back in to continue.

References

Tanaka,  E., 1970, “The Interference of Two-Dimensional Parallel Jets (1st Report, Experiments on Dual Jet),” Bull. JSME, 13(56), p. 272.
Tanaka,  E., 1974, “The Interference of Two-Dimensional Parallel Jets (2nd Report, Experiments on the Combined Flow of Dual Jet),” Bull. JSME, 17(109), p. 920.
Elbanna,  H., Gahin,  S., and Rashed,  M. I. I., 1983, “Investigation of Two Plane Parallel Jets,” AIAA J., 21(7), p. 986.
Lin,  Y. F., and Sheu,  M. J., 1990, “Investigation of Two Plane Parallel Unventilated Jets,” Exp. Fluids, 10, p. 17.
Lin,  Y. F., and Sheu,  M. J., 1991, “Interaction of Parallel Turbulent Plane Jets,” AIAA J., 29, p. 1372.
Nasr,  A., and Lai,  J. C. S., 1997, “Comparison of Flow Characteristics in the Near Field of Two Parallel Plane Jets and an Offset Plane Jet,” Phys. Fluids, 9(10), p. 2919.
Anderson,  E. A., and Spall,  R. E., 2001, “Experimental/Numerical Investigation of Two-Dimensional Parallel Jets,” ASME J. Fluids Eng., 123, p. 401.
Bloor,  M. S., 1964, “The Transition to Turbulence in the Wake of a Circular Cylinder,” J. Fluid Mech., 19, p. 290.
Bearman, P. W., and Tombazis, N., 1992, “The Effects of Three-Dimensional Imposed Disturbances on Bluff-Body Near Wake Flows,” Second International Colloquium on Bluff-Body Aerodynamics and Applications, Melbourne, Australia. Dec. 7–10.

Figures

Grahic Jump Location
Description of parallel jet flowfield parameters and coordinates
Grahic Jump Location
Mean velocity profiles at Red=20,000.d=2.70 cm, ×; d=3.18 cm, +; d=3.81 cm, ○.
Grahic Jump Location
w/d=0.6 jet exit velocity versus fd superimposed over the frequency spectra. Dotted line indicates best linear fit. d=3.18 cm. The log scales for the spectra are hidden.
Grahic Jump Location
Product of shedding frequency and spacer width, fd as a function of jet exit velocity. Lines indicate the best linear fit of data at consistent w/d.
Grahic Jump Location
Relationship between the reduced frequency and w/d

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