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A nonlinear theory of wake development

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Summary

A simple new series, using an expansion of the velocity profile in parabolic cylinder functions, has been developed to describe the nonlinear evolution of a steady, laminar, incompressible wake from a given arbitrary initial profile. The first term in this series is itself found to provide a very satisfactory prediction of the decay of the maximum velocity defect in the wake behind a flat plate or aft of the recirculation zone behind a symmetric blunt body. A detailed analysis, including higher order terms, has been made of the flat plate wake with a Blasius profile at the trailing edge. The same method yields, as a special case, complete results for the development of linearized wakes with arbitrary initial profile under the influence of arbitrary pressure gradients. Finally, for purposes of comparison, a simple approximate solution is obtained using momentum integral methods, and found to predict satisfactorily the decay of the maximum velocity defect.

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References

  1. H. Schlichting,Boundary Layer Theory, McGraw-Hill Book Co., Inc., 1962.

  2. S. Goldstein, Concerning Some Solutions of the Boundary Layer Equations in Hydrodynamics,Proc. of Camb. Phil. Soc., 26, pp. 1–30, 1930.

    Google Scholar 

  3. S. Goldstein, On the Two-dimensional Steady Flow of a Viscous Fluid Behind a Solid Body,Proc. Roy. Soc. London, A 142, 545, 1933.

    Google Scholar 

  4. K. Stewartson, On Asymptotic Expansions in the Theory of Boundary Layers,J. Math. Phys. 36, pp. 173–191, 1957.

    Google Scholar 

  5. A. F. Charwat and J. Der, Studies on Laminar and Turbulent Free Shear Layers with a Finite Initial Boundary Layer at Separation,Proceedings of Conference of Separated Flows, Part I, AGARD C.P. 4, 1966.

  6. A. F. Charwat and L. Schneider, Effect of the Boundary Layer Profile at Separation on the Evolution of the Wake,AIAA J., 5, 6, 1967.

    Google Scholar 

  7. H. Bateman,Higher Transcendental Functions, vol. II, McGraw-Hill Book Co, 1953.

  8. S. H. Hollingdale, Stability and Configuration of the wake produced by Solid Bodies Moving Through Fluids,Philosophical Mag. 7, 29, 1940.

    Google Scholar 

  9. G. Srinivasan, An Experimental Investigation of Turbulent Wakes Behind Two-Dimensional Bodies,M.E. Project Rep. Dept. of Aero. Engg., I.I.Sc., Bangalore, 1966.

  10. A. Prabhu, Incompressible Wake Flow in Pressure Gradient,AIAA J., 4, pp. 925–926, 1966.

    Google Scholar 

  11. H. Gold, Laminar Wake With Arbitrary Initial Profiles,AIAA J., May 1964.

  12. P. G. Hill, “Turbulent Wakes in Pressure Gradients”,M.I.T., Gas Turbine Lab. Rep. 65, 1961.

  13. P. G. Hill, Turbulent Jets in Ducted Streams,J.F.M., 22, 1, pp. 161–186, 1965.

    Google Scholar 

  14. S. Vasantha, Evaluation of Some Integrals Arising in the Solution for the Wake Development from an Arbitrary Initial Profile,Rep 69 FM4, Dept. of Aeronautical Engg. I.I.Sc. 1969.

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Vasantha, S., Narasimha, R. A nonlinear theory of wake development. J Eng Math 4, 51–63 (1970). https://doi.org/10.1007/BF01535179

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