Analysis and Modeling of Pressure Recovery for Separated Reattaching Flows

Author:

Yeung W. W. H.1,Parkinson G. V.2

Affiliation:

1. School of Mechanical and Production Engineering, Nanyang Technological University, Singapore 639798

2. Department of Mechanical Engineering, University of British Columbia, Vancouver, Canada V6T 1Z4

Abstract

Analyses have been carried out on the mean pressure data for separated reattaching flows downstream of a variety of 2-D bluff-bodies to reveal some similarity features. The step height has been identified as an important parameter in relationships such as the correlation between the reattachment length xr and the initial shear-layer angle. The separation velocity (deduced from separation pressure cps) in the direction perpendicular to the upstream flow increases linearly with the reattachment length at fixed step heights. The streamwise location of the vortex center xv (deduced from mean streamline plots) correlates with the location of minimum pressure xm and each varies linearly with the reattachment length. Pressure force, moment and center of pressure induced by the standing vortex also increase with the reattachment length. An inviscid flow model of a rectilinear stationary vortex above a flat wall leads to a general form of the pressure recovery cp−cp min/cp max−cp min)=8/9x^2x^2+1/x^2+1/32xm<,<xr where 0⩽x^1=Xm/Xr and cp max and cp min are respectively the maximum and minimum pressure coefficients. It is demonstrated that the present analyses allow the pressure distributions downstream of various fore-bodies to be realistically predicted.

Publisher

ASME International

Subject

Mechanical Engineering

Reference34 articles.

1. Roshko, A., 1954, “On the drag and shedding frequency of two-dimensional bluff bodies,” NACA Tech. Note 3169.

2. Mansingh, V., and Oosthuizen, P. H., 1990, “Effects of splitter plates on the wake flow behind a bluff body,” AIAA J., 28, pp. 778–783.

3. Fertis, D. G. , 1994, “New airfoil-design concept with improved aerodynamic characteristics,” ASCE, J. Aerosp. Eng., 7, pp. 328–339.

4. Finaish, F., and Witherspoon, S., 1998, “Aerodynamic performance of an airfoil with step-induced vortex for lift augmentation,” ASCE, J. Aerosp. Eng., 11, pp. 9–16.

5. Roshko, A., and Lau, J. C., 1965, “Some Observations on transition and reattachment of a free shear layer in incompressible flow,” Proc. Heat Transfer and Fluid Mech. Inst., Stanford University Press, pp. 157–167.

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