Hostname: page-component-78c5997874-mlc7c Total loading time: 0 Render date: 2024-11-17T09:19:24.526Z Has data issue: false hasContentIssue false

On the stability of a Blasius boundary layer subject to localised suction

Published online by Cambridge University Press:  24 May 2019

Mattias Brynjell-Rahkola*
Affiliation:
KTH Royal Institute of Technology, Linné FLOW Centre and Swedish e-Science Research Centre (SeRC), Department of Mechanics, SE-100 44 Stockholm, Sweden
Ardeshir Hanifi
Affiliation:
KTH Royal Institute of Technology, Linné FLOW Centre and Swedish e-Science Research Centre (SeRC), Department of Mechanics, SE-100 44 Stockholm, Sweden
Dan S. Henningson
Affiliation:
KTH Royal Institute of Technology, Linné FLOW Centre and Swedish e-Science Research Centre (SeRC), Department of Mechanics, SE-100 44 Stockholm, Sweden
*
Email address for correspondence: [email protected]

Abstract

In this study the origins of premature transition due to oversuction in boundary layers are studied. An infinite row of circular suction pipes that are mounted at right angles to a flat plate subject to a Blasius boundary layer is considered. The interaction between the flow originating from neighbouring holes is weak and for the parameters investigated, the pipe is always found to be unsteady regardless of the state of the flow in the boundary layer. A stability analysis reveals that the appearance of boundary layer transition can be associated with a linear instability in the form of two unstable eigenmodes inside the pipe that have weak tails, which extend into the boundary layer. Through an energy budget and a structural sensitivity analysis, the origin of this flow instability is traced to the structures developing inside the pipe near the pipe junction. Although the amplitudes of the modes in the boundary layer are orders of magnitude smaller than the corresponding amplitudes inside the pipe, a Koopman analysis of the data gathered from a nonlinear direct numerical simulation confirms that it is precisely these disturbances that are responsible for transition to turbulence in the boundary layer due to oversuction.

Type
JFM Papers
Copyright
© 2019 Cambridge University Press 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Åkervik, E., Brandt, L., Henningson, D. S., Hœpffner, J., Marxen, O. & Schlatter, P. 2006 Steady solutions of the Navier–Stokes equations by selective frequency damping. Phys. Fluids 18 (6), 068102, 1–4.Google Scholar
Anderson, E., Bai, Z., Bischof, C., Blackford, L., Demmel, J., Dongarra, J., Du Croz, J., Greenbaum, A., Hammarling, S., McKenney, A. & Sorensen, D. 1999 LAPACK Users’ Guide, 3rd edn. Society for Industrial and Applied Mathematics.Google Scholar
Bagheri, S., Åkervik, E., Brandt, L. & Henningson, D. S. 2009 Matrix-free methods for the stability and control of boundary layers. AIAA J. 47 (5), 10571068.Google Scholar
Barkley, D. 2006 Linear analysis of the cylinder wake mean flow. Europhys. Lett. 75 (5), 750756.Google Scholar
Barkley, D., Blackburn, H. M. & Sherwin, S. J. 2008 Direct optimal growth analysis for timesteppers. Intl J. Numer. Meth. Fluids 57 (9), 14351458.Google Scholar
Blanchard, A., Seraudie, A., Breil, J. & Payry, M.1991 Limits of suction through a perforated metal sheet on a model to avoid transition tripping. Tech. Rep. 28/5006.21. ONERA-DERAT.Google Scholar
Brynjell-Rahkola, M., Barman, E., Peplinski, A., Hanifi, A. & Henningson, D. S.2015 On the stability of flat plate boundary layers subject to localized suction. Tech. Rep. Department of Mechanics, KTH Royal Institute of Technology.Google Scholar
Brynjell-Rahkola, M., Shahriari, N., Schlatter, P., Hanifi, A. & Henningson, D. S. 2017 Stability and sensitivity of a cross-flow-dominated Falkner–Skan–Cooke boundary layer with discrete surface roughness. J. Fluid Mech. 826, 830850.Google Scholar
Butler, S. F. J.1955 Current tests on laminar-boundary-layer control by suction through perforations. Tech. Rep. 3040. Aeronautical Research Council Reports and Memoranda.Google Scholar
Chevalier, M., Schlatter, P., Lundbladh, A. & Henningson, D. S.2007 SIMSON – A pseudo-spectral solver for incompressible boundary layer flows. Tech. Rep. TRITA-MEK 2007:07. Department of Mechanics, KTH Royal Institute of Technology.Google Scholar
Chomaz, J.-M. 2005 Global instabilities in spatially developing flows: non-normality and nonlinearity. Annu. Rev. Fluid Mech. 37 (1), 357392.Google Scholar
Fischer, P. F., Lottes, J. W. & Kerkemeier, S. G.2008 nek5000 Web page. https://nek5000.mcs.anl.gov.Google Scholar
Giannetti, F. & Luchini, P. 2007 Structural sensitivity of the first instability of the cylinder wake. J. Fluid Mech. 581, 167197.Google Scholar
Gregory, N. 1961 Research on suction surfaces for laminar flow. In Boundary Layer and Flow Control (ed. Lachmann, G. V.), pp. 924960. Pergamon.Google Scholar
Gregory, N.1962 On critical suction conditions for laminar boundary-layer control by suction into perforations. Tech. Rep. 24, 213. Aeronautical Research Council.Google Scholar
Gregory, N. & Walker, W. S.1955 Experiments on the use of suction through perforated strips for maintaining laminar flow: transition and drag measurements. Tech. Rep. 3083. Aeronautical Research Council Reports and Memoranda.Google Scholar
Heinzel, G., Rüdiger, A. & Schilling, R.2002 Spectrum and spectral density estimation by the discrete Fourier transform (DFT), including a comprehensive list of window functions and some new flat-top windows. Tech. Rep. Max-Planck-Institut für Gravitationsphysik (Albert-Einstein-Institut) Teilinstitut, Hannover.Google Scholar
Hill, D. C. 1995 Adjoint systems and their role in the receptivity problem for boundary layers. J. Fluid Mech. 292, 183204.Google Scholar
Jeong, J. & Hussain, F. 1995 On the identification of a vortex. J. Fluid Mech. 285, 6994.Google Scholar
Joslin, R. D. 1998 Aircraft laminar flow control. Annu. Rev. Fluid Mech. 30 (1), 129.Google Scholar
Lehoucq, R., Sorensen, D. & Yang, C. 1998 ARPACK Users’ Guide. Society for Industrial and Applied Mathematics.Google Scholar
Loiseau, J.-C., Robinet, J.-C., Cherubini, S. & Leriche, E. 2014 Investigation of the roughness-induced transition: global stability analyses and direct numerical simulations. J. Fluid Mech. 760, 175211.Google Scholar
MacManus, D. G. & Eaton, J. A. 1996 Predictions and observations of the flow field induced by laminar flow control microperforations. Exp. Therm. Fluid Sci. 13 (4), 395407; Peter Bradshaw 60th Birthday Issue: Part II.Google Scholar
MacManus, D. G. & Eaton, J. A. 1998 Measurement and analysis of the flowfields induced by suction perforations. AIAA J. 36 (9), 15531561.Google Scholar
MacManus, D. G. & Eaton, J. A. 2000 Flow physics of discrete boundary layer suction – measurements and predictions. J. Fluid Mech. 417, 4775.Google Scholar
Maday, Y. & Patera, A. T. 1989 Spectral element methods for the Navier–Stokes equations. In State of the Art Surveys in Computational Mechanics (ed. Noor, A. K.), pp. 71143. ASME.Google Scholar
Maschhoff, K. J. & Sorensen, D. C. 1996 P_ARPACK: an efficient portable large scale eigenvalue package for distributed memory parallel architectures. In Applied Parallel Computing Industrial Computation and Optimization (ed. Waśniewski, J., Dongarra, J., Madsen, K. & Olesen, D.), pp. 478486. Springer.Google Scholar
Meitz, H. L. & Fasel, H. F. 1994 Navier–Stokes simulations of the effects of suction holes on a flat plate boundary layer. In Application of Direct and Large Eddy Simulation to Transition and Turbulence, AGARD Conference Proceedings 551, Chania/Crete/Greece. AGARD.Google Scholar
Meyer, W. A.1955 Preliminary report on the flow field due to laminar suction through holes. Tech. Rep. NAI-55-290, BLC-75. Northrop Aircraft Inc.Google Scholar
Mezić, I. 2005 Spectral properties of dynamical systems, model reduction and decompositions. Nonlinear Dyn. 41 (1), 309325.Google Scholar
Mezić, I. 2013 Analysis of fluid flows via spectral properties of the Koopman operator. Annu. Rev. Fluid Mech. 45 (1), 357378.Google Scholar
Müller, H.2012 Assessment of roughness analogies for strong discrete suction by means of direct numerical simulation. Master’s thesis, University of Stuttgart.Google Scholar
Patera, A. T. 1984 A spectral element method for fluid dynamics: laminar flow in a channel expansion. J. Comput. Phys. 54 (3), 468488.Google Scholar
Peplinski, A., Schlatter, P. & Henningson, D. S. 2015 Investigations of stability and transition of a jet in crossflow using DNS. In Direct and Large-Eddy Simulation IX (ed. Fröhlich, J., Kuerten, H., Geurts, B. J. & Armenio, V.), pp. 207217. Springer International Publishing.Google Scholar
Rowley, C. W., Mezić, I., Bagheri, S., Schlatter, P. & Henningson, D. S. 2009 Spectral analysis of nonlinear flows. J. Fluid Mech. 641, 115127.Google Scholar
Sarmast, S., Dadfar, R., Mikkelsen, R. F., Schlatter, P., Ivanell, S., Sørensen, J. N. & Henningson, D. S. 2014 Mutual inductance instability of the tip vortices behind a wind turbine. J. Fluid Mech. 755, 705731.Google Scholar
Schlichting, H. 1979 Boundary-Layer Theory, 7th edn. McGraw-Hill, Inc.Google Scholar
Schmid, P. J. 2010 Dynamic mode decomposition of numerical and experimental data. J. Fluid Mech. 656, 528.Google Scholar
Schmid, P. J. & Henningson, D. S. 2001 Stability and Transition in Shear Flows, Applied Mathematical Sciences, vol. 142. Springer.Google Scholar
Schrauf, G. 2005 Status and perspectives of laminar flow. Aeronaut. J. 109 (1102), 639644.Google Scholar
Sipp, D. & Lebedev, A. 2007 Global stability of base and mean flows: a general approach and its applications to cylinder and open cavity flows. J. Fluid Mech. 593, 333358.Google Scholar
Trefethen, L. N. & Bau, D. 1997 Numerical Linear Algebra. Society for Industrial and Applied Mathematics.Google Scholar
Tu, J. H., Rowley, C. W., Luchtenburg, D. M., Brunton, S. L. & Kutz, J. N. 2014 On dynamic mode decomposition: theory and applications. J. Comput. Dyn. 1 (2), 391421.Google Scholar