The Effect of Base Bleed on a Periodic Wake

Author:

Wood C. J.

Abstract

Summary:—Measurements of profile drag, base pressure, wake turbulence and vortex shedding frequency have been made on a 9 per cent thick aerofoil in the presence of a secondary air flow, ejected from the blunt trailing edge. It is shown that the decrease in profile drag caused by the base bleed is associated with a decrease in the strength of the vortex street. The initial formation of the vortices occurs further downstream as the bleed quantity is increased. As a result, a greater proportion of the shed vorticity is diffused before the street is formed.

Publisher

Cambridge University Press (CUP)

Reference10 articles.

1. R.Ae.S. Data Sheets. 02.04.01 and 02.04.02, 1947.

2. Holder D. W. , Pearcey H. H. and Nash J. F. Some Aerodynamic Advantages of Thick Trailing Edges in High Speed Flight. To be published.

3. Nash J. F. A Review of Research on Two-Dimensional Base Flow. A.R.C. 23 649. FM 3171.

4. Bearman P. W. To be published.

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