Skip to main content
SpringerLink
Log in

Turbulent auxiliary functions for symmetric three-dimensional boundary layers

  • Original Papers
  • Published:
Zeitschrift für angewandte Mathematik und Physik ZAMP Aims and scope Submit manuscript

Zusammenfassung

Der allgemeine Charakter der dreidimensionalen Grenzschichtströmung in einem Rotationskörper wird mit Hilfe einer verallgemeinerten Impuls-Integral-Methode untersucht. Die notwendigen Hilfsfunktionen und der Ablösungspunkt der turbulenten Grenzschicht werden durch Einführung geeigneter Formfaktoren bestimmt. Die zweidimensionalen Beziehungen werden dabei unter Berücksichtigung neuerer Versuchsergebnisse umgestaltet und so auf den dreidimensionalen Fall übertragen.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Log in via an institution

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Institutional subscriptions

References

  1. S. L. Soo,Auxiliary Functions of Three-Dimensional Turbulent Boundary Layers, AGARDograph97, 637 (1965).

    Google Scholar 

  2. H. Schlichting,Boundary Layer Theory, McGraw-Hill Book Co., Inc., New York (1960).

    Google Scholar 

  3. J. C. Cooke andM. G. Hall,Boundary Layers in Three Dimensions, AGARD Report 273 (1960).

  4. W. E. Thompson, Jr.,Flow in the Vaneless Diffuser of a Centrifugal Compressor, Ph. D. Thesis, Illinois Institute of Technology (1958).

  5. E. B. Gardow,The Three-Dimensional Boundary Layer in a Free Vortex Diffuser, M. S. Thesis, Massachusetts Institute of Technology, Cambridge, Mass. (1958).

    Google Scholar 

  6. W. B. Brown,Friction Coefficients in Vaneless Diffuser, NACA TN 1311 (1947).

  7. B. S. Stratford andG. S. Beavers,The Calculation of Compressible Turbulent Boundary Layer in an Arbitrary Pressure Gradient: A Correlation of Certain Previous Methods, Reports and Memoranda (Ministry of Supply, U.K.), No. 3207 (1959).

  8. D. Coles,The Turbulent Boundary Layer in a Compressible Fluid, Phys. Fluids7, No. 9, 1403–1423 (1964).

    Google Scholar 

  9. B. S. Stratford,An Experimental Flow with Zero Skin Friction Throughout Its Regime of Pressure Rise, J. Fluid Mech.5, 17 (1959).

    Google Scholar 

Download references

Author information

Authors and Affiliations

  1. Dpt. of Mechanical Engineering, University of Illinois, Urbana, Illinois, USA

    Shao L. Soo

Authors
  1. Shao L. Soo
    View author publications

    You can also search for this author in PubMed Google Scholar

Rights and permissions

Reprints and permissions

About this article

Cite this article

Soo, S.L. Turbulent auxiliary functions for symmetric three-dimensional boundary layers. Journal of Applied Mathematics and Physics (ZAMP) 17, 122–131 (1966). https://doi.org/10.1007/BF01594091

Download citation

  • Received:

  • Issue Date:

  • DOI: https://doi.org/10.1007/BF01594091

Keywords

Search

Navigation