Some Experiments on the Reattachment of a Laminar Boundary Layer Separating From a Rearward Facing Step on a Flat Plate Aerofoil

Author:

Moore T. W. F.

Abstract

Summary:The results of experiments on the reattachment of a laminar boundary layer, separating from a rearward facing step in a flat plate aerofoil, are correlated with the properties of the short leading edge bubble which forms on thin aerofoils near the stall.The experiments, comprising pressure measurements, Pitot explorations, liquid film and smoke studies, indicate that for all Reynolds numbers above the value given by the Owen-KIanfer criterion the reattachment is turbulent behind a stationary air reverse flow vortex bubble. It is also found that the reattachment is laminar for Reynolds numbers below the critical, which further supports Crabtree's interpretation of the Owen-KIanfer criterion in terms of the condition for the growth of turbulent bursts.

Publisher

Cambridge University Press (CUP)

Reference4 articles.

1. Crabtree L. F. (1957). The formation of regions of separated flow on wing surfaces. Part II Laminar separation bubbles and the mechanism of the leading-edge stall. R.A.E. Report 2578. 1957.

2. A Note on the Causes of Thin Aerofoil Stall

3. Owen P. R. and Klanfer L. (1953). On the laminar boundary layer separation from the leading edge of a thin aerofoil. A.R.C. C.P.220. October 1953.

4. Effects of Leading-Edge Separation on Thin Wings in Two-Dimensional Incompressible Flow

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