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The Effect of Small-Scale Roughness on the Mean Flow Profile of a Laminar Boundary Layer

  • James M. Kendall
Part of the ICASE/NASA LaRC Series book series (ICASE/NASA)

Abstract

The processes by which distributed surface roughness accelerate boundary layer transition remain unclear. Experimental studies aimed at clarification were carried out during the early 1980s by three groups who maintained intercommunication. In each case, Blasius-like boundary layers were selected for study for reasons of simplicity and standardization. The experiments by Leventhal [1] and by Corke, Bar-Sever, and Morkovin [2] concerned measurement of the growth of naturally-occurring flow fluctuations within laminar layers during passage over sandpaper roughness. In contrast, this author [3] chose to measure only the mean velocity alteration due to roughness, with the expectation that the distorted profile could be analyzed for incremental growth using stability theory.

Keywords

Laminar Boundary Layer Vortex Pair Boundary Layer Transition Distorted Profile Roughness Density 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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References

  1. [1]
    Leventhal, L., “Preliminary Experimental Study of Disturbances in a Laminar Boundary Layer Due to Distributed Surface Roughness,” M.S. Thesis, Case Western Reserve University, Cleveland, OH, December 1980.Google Scholar
  2. [2]
    Corke, T. C., Bar-Sever, A., and Morkovin, M. V., “Experiments on Transition Enhancement by Distributed Roughness,” Phys. Fluids, Vol. 29, No. 10, pp. 3199 – 3213, 1986.ADSCrossRefGoogle Scholar
  3. [3]
    Kendall, J. M., “Laminar Boundary Layer Velocity Distortion by Surface Roughness: Effect upon Stability,” AIAA Paper 81–0195, St. Louis, January, 1981.Google Scholar

Copyright information

© Springer-Verlag New York Inc. 1990

Authors and Affiliations

  • James M. Kendall
    • 1
  1. 1.Jet Propulsion LaboratoryPasadenaUSA

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