Separation in oscillating laminar boundary-layer flows

Author:

Despard R. A.,Miller J. A.

Abstract

The results of an experimental investigation of separation in oscillating laminar boundary layers is reported. Instantaneous velocity profiles obtained with multiple hot-wire anemometer arrays reveal that the onset of wake formation is preceded by the initial vanishing of shear at the wall, or reverse flow, throughout the entire cycle of oscillation. Correlation of the experimental data indicates that the frequency, Reynolds number and dynamic history of the boundary layer are the dominant parameters and oscillation amplitude has a negligible effect on separation-point displacement.

Publisher

Cambridge University Press (CUP)

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference12 articles.

1. Moore, F. K. 1958 On separation of the unsteady laminar boundary layer. Boundary Layer Research Symposium Frieburg ,Germany,Springer-Verlag.

2. Sandborn, V. A. 1969 Characteristics of boundary layers at separation and reattachments.Res. Memo. no. 14 College of Engineering, Colorado State University.

3. Moore, F. K. 1955 Lift hysteresis at stall as an unsteady boundary-layer phenomena.NACA Tech. Note 3571.

4. Stuart, J. T. 1963 Periodic boundary layers. In Laminar Boundary Layers , part II (ed. L. Rosenhead ) chapter VII.Oxford University Press.

5. Hill, P. G. 1958 Laminar boundary layers in oscillatory flow. Sc.D. Thesis,Massachusetts Institute of Technology.

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