Fluid Flow Structures in Staggered Banks of Cylinders Located in a Channel

Author:

Braun M. J.1,Kudriavtsev V. V.2

Affiliation:

1. Department of Mechanical Engineering, The University of Akron, Akron, OH 44325

2. Department of Mechanical Engineering, The University of Akron/Moscow Aviation Institute, School of Engine Technology, Russia

Abstract

This paper contains numerical experiments that model fluid flow through a staggered array of cylinders and represents a continuation of work previously performed by the authors (Braun et al., 1993; Kudriavstsev et al., 1993). The results shown here concentrate on the analysis of the physics of flow and pressure distribution in (i) one row of cylinders, and (ii) seven rows of cylinders. The test section is the same square channel described by Braun et al. (1993). The numerical experiments were run in transient mode at Reynolds numbers (Re = umaxd/v) ranging from 86 to 869. The primary purpose of this paper is to report qualitative results regarding the attached near-wall jet phenomenon and to discuss its flow mechanics. The authors compare various stages of the transient evolution of the flow structures for geometric configurations that contain one, and seven rows of pins respectively. The associated pressure distributions in the arrays of pins are also discussed.

Publisher

ASME International

Subject

Mechanical Engineering

Reference17 articles.

1. Braun, M. J., and Kudriavtsev, V. V., 1993, “A Numerical Simulation of a Brush Seal Section and Some Experimental Results,” International Gas Turbine and AeroEngine Congress, Cincinnati, ASME Paper 93-GT-387, pp. 1–12 (accepted for the publication in the ASME Journal of Turbomachinery, Feb. 1995).

2. Braun, M. J., and Kudriavtsev, V. V., 1992, “Experimental and Analytical Investigation of Brush Seals,” Seals Flow Code Development-92, NASA CP-10124, Proceedings of a workshop held at NASA Lewis Research Center, Aug. 5–6, pp. 181–195.

3. Bouard R. , and CoutanceauM., 1980, “The Early Stage of Development of the Wake Behind an Impulsively Started Cylinder for 40 < Re < 104,” Journal of Fluid Mechanics, Vol. 101, Part 3, pp. 583583.

4. Chen, C. K., Wong, K. L., and Cleaver, J. W., 1986, “Finite Element Solution of Laminar and Heat Transfer of Air in a Staggered and In-Line Tube Bank,” International Heat and Fluid Flow, No. 4, p. 291.

5. Fornberg B. , 1991, “Steady Incompressible Flow Past a Row of Circular Cylinders,” Journal of Fluid Mechanics, Vol. 225, pp. 655–671.

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