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Application of VITA technique for detection of the organized structures present in a turbulent boundary layer under an adverse pressure gradient

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Języki publikacji
EN
Abstrakty
EN
The paper concerns experimental investigations of turbulent boundary layer (TBL), developing on a flat plate at Reynolds number based on momentum thickness= 3000 under an adverse pressure gradient (APG) corresponding to the case of pressure variation at axial compressor blading. In particular, the paper deals with the analysis of bursting phenomena and coherent structures activity in TBL with the use of VITA technique. The interpretation of coherent structures was based on the analysis of conditionally averaged traces of u and v velocity components recorded by X-wire probe in several boundary layer regions. The paper describes the modification introduced into the VITA method, which enables to distinguish four types of coherent structures. This modification relies on the detection of instantaneous positive or negative gradients of u and v velocity traces. It was found that bursting process under the influence of adverse pressure gradient is damped near the wall and this phenomenon is even more pronounced in the outer region of turbulent boundary layer. Furthermore, the paper gives the consistent proof, that vortices developing in TBL create the effect of bursting present in velocity signal.
Rocznik
Strony
183--199
Opis fizyczny
Bibliogr. 13 poz.
Twórcy
autor
autor
autor
  • Institute of Thermal Machinery, Czestochowa University of Technology Al. Armii Krajowej 21 42-201 Częstochowa, Poland, arturdr@imc.pcz.czest.pl,
Bibliografia
  • 1. R.F. Blackwelder, R.E. Kaplan, On the wall structure of the turbulent Bondary layer, J. Fluid Mech., 76, 89–112, 1976.
  • 2. T. Teodorsen, Mechanism of turbulence, [in:] Proc. 2nd Midwestern Conference on Fluid Mechanics, Ohio State University, Columbus, Ohio, 1–19, 1952.
  • 3. H.T. Kim, S.J. Kline, W.C. Reynolds, The production of turbulence near a smooth wall in a turbulent boundary layer, J. Fluid Mech., 50, 133–160, 1971.
  • 4. E.R. Corino, R.S. Brodkey, A visual observation of the wall region in turbulent flow, J. Fluid Mech., 37, 1–30, 1969.
  • 5. R.J. Adrian, Hairpin vortex organization in wall turbulence, Phys. Fluids, 19, 041301, 2007.
  • 6. V.K. Natrajan, Y. Wu, K.T. Christensen, Spatial signatures of retrograde spanwise vortices in wall turbulence, J. Fluid Mech. 574, 155–167, 2007.
  • 7. P.A. Krogstad, P.E. Skare, Influence of a strong adverse pressure gradient on the turbulent structure in boundary layer, Phys. Fluids, vol. 7, No 8, 1995.
  • 8. M. Materny, A. Dróżdż, S. Drobniak, W. Elsner, Experimental analysis of turbulent boundary layer under the influence of adverse pressure gradient, Arch. Mech., 60, 449–466, 2008.
  • 9. S. Drobniak, W. Elsner, A. Dróżdż, M. Materny-Latos, Experimental analysis of turbulent boundary layer with adverse pressure gradient corresponding to turbomachinery condition, Proc. of Workshop “Progress in wall turbulence: understanding and modelling”, 21–23 April, Springer, 141–148, 2009.
  • 10. F.J. Keller, T. Wang, Effects of criterion functions on intermittency in heated transitional boundary layers with and without streamwise acceleration, Trans. of ASME, 117, January 1995.
  • 11. R.J. Adrian, C.D. Meinhart, C.D. Tomkins, Vortex organization in the outer region of the turbulent boundary layer, J. Fluid Mech., 422, 1–54, 2000.
  • 12. M. Ichimiya, I. Ikuo Nakamura, S. Yamashita, Properties of a relaminarizing turbulent boundary layer under a favorable pressure gradient, Experimental Thermal and Fluid Science, 17, 37–48, 1998.
  • 13. M. Stanislas, J. Jimenez, I. Marusic, Progress in Wall Turbulence: Understanding and Modeling, Springer ERCOFTAC Series, Vol. 14, 2010.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BAT4-0010-0017
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