Advertisement

Measurements in an axisymmetric turbulent boundary layer with weak and strong three-dimensional disturbances

  • H. H. Fernholz
  • J. -D. Vagt
Conference paper
Part of the Lecture Notes in Physics book series (LNP, volume 75)

Keywords

Boundary Layer Test Section Circular Cylinder Skin Friction Turbulent Boundary Layer 
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.

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  1. 1.
    Vagt, J.-D.: Bemerkungen zur Auslegung eines Unterschallfrei-strahl-Windkanals. Z.f.W. 21 (1973), 159–162.Google Scholar
  2. 2.
    Patel, V.C.: Calibration of the Preston tube and limitations its use in pressure gradients. J. Fluid Mech. 23 (1965), 1853Google Scholar
  3. 3.
    Vagt, J.-D.; Dahm, A.: Interferenzarme Hi tzdrahtsonden DLR-SB 16, 1977.Google Scholar
  4. 4.
    Dahm, A.; Vagt, J.-D.: Entwicklung und Herstellung interferer armer Hitzdrahtsonden. Hermann-Föttinger-Institut für Thermo-und Fluiddynamik Institutsbericht 01/77 (1977).Google Scholar
  5. 5.
    Vagt, J.-D.; Fernholz, H.H.: Use of surface fences to measure wall shear stress in three-dimensional baundary layers. J. Aeronaut. Quart. XXIV (1973), 87–91.Google Scholar
  6. 6.
    Head, M.R.; Rechenberg, I.: The preston tube as a means of measuring skin friction. J. Fluid Mech. 14 (1962), 1–17.Google Scholar
  7. 7.
    Fernholz, H.H.: Three-dimensional disturbances in a two-dimensional incompressible turbulent boundary layer. A.R.C. London R + M 3368 (1964).Google Scholar
  8. 8.
    de Bray, B.G.: Some investigations into the spanwise non-uniformity of nominally two-dimensional incompressible boundary layers downstream of gauze screens. A.R.C. London R + M 3578Google Scholar
  9. 9.
    Bradshaw, P.: The effect of wind tunnel screens on “two-dimentional” boundary layers. NPL Aero Rep. 1085 (1963).Google Scholar
  10. 10.
    Pozzorini, R.: Das turbulente Strömungsfeld in einem langen Kreiskegeldiffusor. Dissertation ETH 5646 Zürich (1976).Google Scholar
  11. 11.
    Hassler, H.: Experimentelle Untersuchung von Längswirbeln im vorderen Staupunktgebiet eines Kreiskegels in axialsymmetrischer Anströmung. DLR FB 76-31 (1976).Google Scholar
  12. 12.
    Winkelmann, A.E.; Melnik, W.L.: An experimental investigation of a two and a three-dimensional low speed turbulent boundary layer. University of Maryland, Dept. Aerospace Eng. TR AE-76. (1976).Google Scholar
  13. 13.
    Schlichting, H.: Grenzschicht-Theorie. Verlag G. Braun Karlsruhe 5. Aufl. (1965).Google Scholar
  14. 14.
    Bradshaw, P.: Experimental Fluid Mechanics. Pergamon Press 1970 second edition.Google Scholar
  15. 15.
    Piercy, N.A.V.; Richardson, E.G.: On the flow of air adjacent to the surface of an aerofoil. ARC R + M 1224 (1928).Google Scholar
  16. 16.
    Piercy, N.A.V.; Richardson, E.G.: The variation of velocity amplitude close to the surface of a cylinder moving through a viscous fluid. Phil. Mag. Ser. 7 6 (1928), 970–977.Google Scholar
  17. 17.
    Bissonnette, L.R.; Mellor, G.L.: Experiments on the behaviour of an axisymmetric boundary layer with a sudden circumferential strain. J. Fluid Mech. 63 (1974) 369–413.Google Scholar
  18. 18.
    Bradshaw, P.; Unsworth, K.: An improved Fortran program for the Bradshaw-Ferriss-Atwell method of calculating turbulent shear layers. Imperial College Aero. Rep. 74-02 (1974).Google Scholar
  19. 19.
    Froebel, E.; Vagt, J.-D.: Ein automatisch abgleichendes Flussigkeitsmanometer mit digitaler Anzeige. DLR-FB 74-40 (1974).Google Scholar

Copyright information

© Springer-Verlag 1978

Authors and Affiliations

  • H. H. Fernholz
    • 1
  • J. -D. Vagt
    • 1
  1. 1.Hermann-Föttinger-InstitutTechnische UniversitätBerlin

Personalised recommendations