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Wake instabilities of a blunt trailing edge profiled body at intermediate Reynolds numbers

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Abstract

Experiments have been conducted to identify and characterize the instabilities in the wake of a blunt trailing edge profiled body, comprised of an elliptical leading edge and a rectangular trailing edge, for a broad range of Reynolds numbers (\(2{,}000\le Re(d)\le 50{,}000\) based on the thickness of the body). These experiments, which include measurements of the wake velocity field using hot-wire anemometry and particle image velocimetry, complement previous studies of the wake flow for the same geometry at lower and higher Reynolds numbers. The spatial characteristics of the primary wake instability (the von Kármán vortex street) are found to have relatively little variation in the range of Reynolds numbers investigated, in spite of the transition of the boundary layer upstream of the trailing edge from a laminar to a turbulent state. The dominant secondary instability, identified based on the structure of velocity and vorticity fields in the wake extracted using proper orthogonal decomposition, is found to have features similar to the ones described numerically and experimentally by Ryan et al. (J Fluid Mech 538:1–29, 2005), and Naghib-Lahouti et al. (Exp Fluids 52:1547–1566, 2012) at lower Reynolds numbers. The findings suggest that the spatial characteristics of the dominant primary and secondary wake flow instabilities have little dependence on the state of the flow upstream of the separation points, in spite of the distinct change in the normalized vortex shedding frequency upon the transition of the boundary layer.

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References

  • Baker J, Mayda E, van Dam C (2006) Experimental analysis of thick blunt trailing-edge wind turbine airfoils. J Sol Energy Eng 128:422–431

    Article  Google Scholar 

  • Bays-Muchmore B, Ahmed A (1993) On streamwise vortices in turbulent wakes of cylinders. Phys Fluids 5(2):387–392

    Article  Google Scholar 

  • Bearman P (1971) Corrections for the effect of ambient temperature drift on hot-wire measurements in incompressible flows. DISA Information 11, Dantec Dynamics, Skovlunde, Denmark

  • Bearman P, Tombazis N (1993) The effects of three-dimensional imposed disturbances on bluff body near-wake flows. J Wind Eng Ind Aerodyn 49:339–350

    Article  Google Scholar 

  • Brede M, Eckelmann H, Rockwell D (1996) On secondary vortices in the cylinder wake. Phys Fluids 8(8):2117–2124

    Article  Google Scholar 

  • Bull M, Li Y, Pickles J (1995) Effects of boundary layer transition on vortex shedding from thick plates with faired leading edge and square trailing edge. In: Proceedings of the 12th Australasian fluid mechanics conference, Australia, Sydney, pp 231–234

  • Cowen E, Monismith S (1997) A hybrid digital particle tracking velocimetry technique. Exp Fluids 22:199–211

    Article  Google Scholar 

  • Dobre A, Hangan H (2004) Investigation of the three-dimensional intermediate wake topology for a square cylinder at high Reynolds number. Exp Fluids 37:518–530

    Article  Google Scholar 

  • Doddipatla L (2010) Wake dynamics and passive flow control of a blunt trailing edge profiled body. PhD thesis, The University of Western Ontario, London, Canada

  • Eisenlohr E, Eckelmann H (1988) Observations in the laminar wake of a thin flat plate with a blunt trailing edge. In: Proceedings of the conference on experimental heat transfer, fluid mechanics, and thermodynamics, Dubrovnik, Yugoslavia, pp 264–268

  • El-Gammal M, Hangan H (2008) Three-dimensional wake dynamics of a blunt and divergent trailing edge airfoil. Exp Fluids 44:705–717

    Article  Google Scholar 

  • Hangan H, Kopp G, Vernet A, Martinuzzi R (2001) A wavelet pattern recognition technique for identifying flow structures in cylinder generated wakes. J Wind Eng Ind Aerodyn 89:1001–1015

    Article  Google Scholar 

  • Hourigan K, Thompson M, Sheard G, Ryan K, Leontini J, Johnson SA (2007) Low Reynolds number instabilities and transitions in bluff body wakes. J Phys Conf Ser 64:1–10

    Article  Google Scholar 

  • Jorgensen F (2002) How to measure turbulence with hotwire anemometers. Publication 9040U6151, Dantec Dynamics, Skovlunde, Denmark

  • Lin J, Vorobieff P, Rockwell D (1995) Three dimensional patterns of streamwise vorticity in the turbulent near wake of a circular cylinder. J Fluids Struct 9:231–234

    Article  Google Scholar 

  • Mansy H, Yang P, Williams D (1994) Quantitative measurements of three-dimensional structures in the wake of a circular cylinder. J Fluid Mech 270:277–296

    Article  Google Scholar 

  • Miller I, Shah D, Antonia R (1987) A constant temperature hot-wire anemometer. J Phys E Conf Ser 20:311–314

    Article  Google Scholar 

  • Moffat R (1988) Describing uncertainties in experimental results. Exp Therm Fluid Sci 1(1):3–17

    Article  Google Scholar 

  • Naghib-Lahouti A, Doddipatla L, Hangan H (2012) Secondary wake instabilities of a blunt trailing edge profiled body as a basis for flow control. Exp Fluids 52:1547–1566

    Article  Google Scholar 

  • Niebles-Atencio B, Chernoray V, Jahanmiri M (2012) An experimental study on laminar–turbulent transition at high free-stream turbulence in boundary layers with pressure gradients. In: Wang AB, Fraunie P (eds) Proceedings of EFM11—experimental fluid mechanics 2011, EPJ Web of conferences, vol 25, p id.01029

  • Oertel H (1990) Wakes behind blunt bodies. Annu Rev Fluid Mech 22:539–564

    Article  MathSciNet  Google Scholar 

  • Park H, Lee D, Jeon W, Hahn S, Kim J, Choi J, Choi H (2006) Drag reduction in flow over a two-dimensional bluff body with a blunt trailing edge using a new passive device. J Fluid Mech 563:389–414

    Article  MATH  Google Scholar 

  • Pastoor M, Henning L, Noack B, King R, Tadmor G (2008) Feedback shear layer control for bluff body drag reduction. J Fluid Mech 608:161–196

    Article  MATH  Google Scholar 

  • Petrusma M, Gai S (1996) Bluff body wakes with free, fixed, and discontinuous separation at low Reynolds numbers and low aspect ratio. Exp Fluids 10:189–198

    Google Scholar 

  • Robichaux J, Balachandar S, Vanka S (1999) Three-dimensional Floquet instability of the wake of square cylinder. Phys Fluids 11(3):560–578

    Article  MATH  MathSciNet  Google Scholar 

  • Roshko A (1954) On the development of turbulent wakes from vortex streets. Report 1911, National Advisory Committee for Aeronautics

  • Ryan K, Thompson M, Hourigan K (2005) Three-dimensional transition in the wake of bluff elongated cylinders. J Fluid Mech 538:1–29

    Article  MATH  Google Scholar 

  • Schlichting H (1979) Boundary-layer theory, 7th edn. McGraw-Hill Inc., New York

    MATH  Google Scholar 

  • Sheard G (2007) Cylinders with elliptic cross-section: Wake stability with variation in angle of incidence. In: Proceedings of IUTAM symposium on unsteady separated flows and their control, Korfu, Greece

  • Sheard G, Fitzgerald M, Ryan K (2009) Cylinders with square cross-section: wake instabilities with incidence angle variation. J Fluid Mech 630:43–69

    Article  MATH  Google Scholar 

  • Sirovich L (1987) Turbulence and dynamics of coherent structures. Q Appl Math 45:561–590

    MATH  MathSciNet  Google Scholar 

  • Williamson C (1996) Vortex dynamics in the cylinder wake. Annu Rev Fluid Mech 28:477–539

    Article  Google Scholar 

  • Wu J, Sheridan J, Welsh M, Hourigan K (1996) Three-dimensional vortex structures in a cylinder wake. J Fluid Mech 312:201–222

    Article  MathSciNet  Google Scholar 

  • Yen S, Yang C (2011) Flow patterns and vortex shedding behavior behind a square cylinder. J Wind Eng Ind Aerodyn 99:868–878

    Article  Google Scholar 

Download references

Acknowledgments

The authors would like to acknowledge the financial support of the Natural Sciences and Engineering Research Council of Canada, Mitacs Inc., and the Ontario Ministry of Research and Innovation.

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Correspondence to A. Naghib-Lahouti.

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Naghib-Lahouti, A., Lavoie, P. & Hangan, H. Wake instabilities of a blunt trailing edge profiled body at intermediate Reynolds numbers. Exp Fluids 55, 1779 (2014). https://doi.org/10.1007/s00348-014-1779-4

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  • DOI: https://doi.org/10.1007/s00348-014-1779-4

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