The flat plate boundary layer. Part 2. The effect of increasing thickness on stability

Author:

Barry M. D. J.,Ross M. A. S.

Abstract

Numerical analysis has been used to find the neutral stability curve for the flat plate boundary layer in zero pressure gradient when the main terms representing the growth of boundary-layer thickness are either included or excluded. The boundary layer is found to be slightly less stable when the extra terms are included. The calculations give a critical Reynolds number of 500.

Publisher

Cambridge University Press (CUP)

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference8 articles.

1. Wazzan, A. R. , Okamura, T. T. & Smith, A. M. O. 1968 Douglas Aircraft Company, Report no. DAC-67086.

2. Ross, J. A. , Barnes, F. H. , Burns, J. G. & Ross, M. A. S. 1970 J. Fluid Mech. 43,81.

3. Jones, C. W. & Watson, E. J. 1963 In Laminar Boundary Layers .Oxford University Press.

4. Schubauer, H. B. & Skramstad, H. K. 1947 J. Res. Nat. Bur. Stand. 38,25.

5. Kaplan, R. E. 1964 ASRL-TR-116–1 Cambridge Aerolastic and Structures Lab. Rep., M.I.T.

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