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The Effect of Pressure Gradient on Boundary Layer Receptivity

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Abstract

This paper presents numerical results for the receptivity of three laminar boundary layers with zero (ZPG), adverse (APG) and favourable (FPG) pressure gradients. Each boundary layer is subjected to a series of simple freestream waveforms which can be considered as constituent parts of either an isotropic or a non-isotropic turbulent freestream. Each freestream waveform has a single frequency in each spatial direction and is divided into two mutually perpendicular components. The first component has a zero spanwise velocity and hence lies in the streamwise normal plane whereas the second component lies in a plane which is perpendicular both to this plane and the spatial frequency vector. High boundary layer receptivities are only obtained for a minority of these waveforms and so only the resulting flow structures for these waveforms are considered in detail. The dominant flow structures are identified as either Tollmien Schlichting (T-S) waves or streaky structures. The streaky structures can be induced by both freestream components, but the response to the second component, which results in streamwise vortices in the freestream, is considerably stronger and occurs over a much larger streamwise frequency range. The boundary layer is only receptive to a relatively narrow band of spanwise wavelengths ranging from approximately one to four times the local boundary layer thickness. The APG leads to receptivities which are more than double those for the FPG case. The ratio of the freestream fluctuation streamwise wavelength to the distance from the plate leading edge is identified as an important influential parameter for receptivity leading to streaks. Significant T-S activity is only observed for APG, but is also detected for ZPG.

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References

  1. Abu-Ghannam, B.J., Shaw, R.: Natural transition of boundary layers—the effects of turbulence, pressure gradient and flow history. J. Mech. Eng. Sci. 22, 213–228 (1980)

    Article  Google Scholar 

  2. Jacobs, R.G., Durbin, P.A.: Simulations of bypass transition. J. Fluid Mech. 428, 185–212 (2001)

    Article  MATH  Google Scholar 

  3. Matsubara, M., Alfredsson, P.H.: Disturbance growth in boundary layers subjected to free-stream turbulence. J. Fluid Mech. 430, 149–168 (2001)

    Article  MATH  Google Scholar 

  4. Mandal, A.C., Venkatakrishnan, L., Dey, J.: A study on boundary-layer transition induced by free-stream turbulence. J. Fluid Mech. 660, 114–146 (2010)

    Article  MATH  Google Scholar 

  5. Nolan, K.P., Walsh, E.J.: Particle image velocimetry measurements of a transitional boundary layer under free stream turbulence. J. Fluid Mech. 702, 215–238 (2012)

    Article  MATH  Google Scholar 

  6. Morkovin, M.V.: On the many faces of transition. In: Wells, C.S. (ed.) Viscous Drag Reduction, p. 412. Plenum, NY (1969)

  7. Hughes, J.D., Walker, G.J.: Natural transition phenomena on an axial compressor blade. J. Turbomach. 123, 392–401 (2001)

    Article  Google Scholar 

  8. Zaki, T.A., Wissink, J.G., Rodi, W., Durbin, P.A.: Direct numerical simulation of transition in a compressor cascade: influence of free-stream turbulence. J. Fluid Mech. 665, 57–98 (2010)

    Article  MATH  Google Scholar 

  9. Liu, Y., Zaki, T.A., Durbin, P.A.: Boundary layer transition by interaction of discrete and continuous modes. J. Fluid Mech. 604, 199–233 (2008)

    Article  MATH  MathSciNet  Google Scholar 

  10. Fasel, H.F.: Numerical investigation of the interaction of the Klebanoff-mode with a Tollmien-Schlichting wave. J. Fluid Mech. 450, 1–33 (2002)

    MATH  MathSciNet  Google Scholar 

  11. Fransson, J.H.M., Brandt, L., Talamelli, A., Cossu, C.: Experimental study of the stabilisation of Tollmein-Schlichting waves by finite amplitude streaks. Phys. Fluids, 17 (2005)

  12. Goldstein, M.E., Sescu, A.: Boundary layer transition at high free-stream disturbance levels—beyond Klebanoff modes. J. Fluid Mech. 613, 95–124 (2008)

    Article  MATH  MathSciNet  Google Scholar 

  13. Vaughan, N.J., Zaki, T.A.: Stability of zero-pressure-gradient boundary layer distorted by unsteady Klebanoff streaks. J. Fluid Mech. 681, 116–153 (2011)

    Article  MATH  Google Scholar 

  14. Zaki, T.A., Durbin, P.A.: Mode interaction and the bypass route to transition. J. Fluid Mech. 531, 85–111 (2005)

    Article  MATH  MathSciNet  Google Scholar 

  15. Zaki, T.A., Durbin, P.A.: Continuous mode transition and the effects of pressure gradient. J. Fluid Mech. 563, 357–388 (2006)

    Article  MATH  MathSciNet  Google Scholar 

  16. Johnson, M.W., Ercan, A.H.: A physical model for bypass transition. Int. J. Heat Fluid Flow 20, 95–104 (1999)

    Article  Google Scholar 

  17. Andersson, P., Berggren, M., Henningson, D.S.: Optimal disturbances and bypass transition in boundary layers. Phys. Fluids 11, 134–150 (1999)

    Article  MATH  MathSciNet  Google Scholar 

  18. Tollmien, W. Uber die Entstehung der Turbulenz. 1 Mitteilung, nachr. Ges. Wiss. Gottingen. Math. Phys. Klasse 21–44, 1929; Engl. Transl. in NACA TM 609 (1931)

  19. Schubauer, G.B., Skramstad, H.K.: Laminar boundary layer oscillations and stability of laminar flow. National Bureau of Standards Research Paper 1772, Reprint of Confidential NACA Report (1943)

  20. Luchini, P.: Reynolds-number-independent instability of the boundary layer over a flat surface: optimal perturbations. J. Fluid Mech. 404, 289–309 (2000)

    Article  MATH  MathSciNet  Google Scholar 

  21. Schlatter, P., Brandt, L., de Lange, H.C., Henningson, D.S.: On streak breakdown in bypass transition. Phys. Fluids 20 (2008). Article No. 101505

  22. Liu, Y., Zaki, T.A., Durbin, P.A.: Floquet analysis of secondary instability of boundary layers distorted by Klebanoff streaks and Tollmien-Schlichting waves. Phys. Fluids 20 (2008). Article No. 124102

  23. Templemann, D., Hanifi, A., Henningson, D.S.: Spatial optimal growth in three-dimensional compressible boundary layers. J. Fluid Mech. 704, 251–279 (2012)

    Article  MathSciNet  Google Scholar 

  24. Leib, S.J., Wundrow, D.W., Goldstein, M.E.: Effect of free-stream turbulence and other vortical disturbances on a laminar boundary layer. J. Fluid Mech. 380, 169–203 (1999)

    Article  MATH  MathSciNet  Google Scholar 

  25. Ricco, P., Wu, X.: Response of a compressible laminar boundary layer to free-stream vortical disturbances. J. Fluid Mech. 587, 97–138 (2007)

    Article  MATH  MathSciNet  Google Scholar 

  26. Mayle, R.E.: The role of laminar-turbulent transition in gas turbine engines. ASME J. Turbomach. 113, 509–537 (1991)

    Article  Google Scholar 

  27. Westin, K.J.A., Boiko, A.V., Klingmann, B.G.B., Kozlov, V.V., Alfredsson, P.H.: Experiments in a boundary layer subjected to free stream turbulence. Part 1. Boundary layer strucuture and receptivity. J. Fluid Mech. 281, 193–218 (1994)

    Article  Google Scholar 

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Correspondence to Mark W. Johnson.

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Johnson, M.W., Pinarbasi, A. The Effect of Pressure Gradient on Boundary Layer Receptivity. Flow Turbulence Combust 93, 1–24 (2014). https://doi.org/10.1007/s10494-014-9529-5

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