Abstract
One of the possible forcing mechanisms for inducing transition from laminar to turbulent flow is freestream turbulence. Among the different transition mechanisms, freestream turbulence influences the cross-flow instability which occurs on swept wings. In order to understand better the physical interaction between freestream turbulence and boundary layer, this work analyses how the turbulence is distorted approaching a leading edge and whether it is amplified approaching a swept leading edge. The paper contains a brief literature review of both the two-dimensional stagnation point and three-dimensional attachment-line flows. This reveals that freestream turbulence amplification has been investigated for two-dimensional leading edge flows, but there is a lack of research on the swept leading edge. In addition, the paper presents some experimental results on a circular cylinder at various sweep angles. The results show that the phenomenon observed at the two-dimensional stagnation point also occurs at a swept attachment-line, although some differences are identified.
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References
Saric, W.S., Reed, H.L., White, E.B.: Stability and transition of three-dimensional boundary layers. Annual Review of Fluid Mechanics 35, 413–440 (2003)
Bippes, H., Mueller, B.: Experiments on the laminar-turbulent transition on swept wings. NASA STI/Recon Technical Report 90, 3–16 (1988)
White, E., Saric, W., Gladden, R., Gabet, P. (2001). Stages of swept-wing transition. 39th Aerospace Sciences Meeting and Exhibit, p. 271
Downs, R.S., White, E.B.: Free-stream turbulence and the development of cross-flow disturbances. Journal of Fluid Mechanics 735, 347–380 (2013)
Kurian, T., Fransson, J. H., Alfredsson, P. H. (2011). Boundary layer receptivity to free-stream turbulence and surface roughness over a swept flat plate. Physics of Fluids, 23
Borodulin, V.I., Ivanov, A.V., Kachanov, Y.S.: Swept-wing boundary-layer transition at various external perturbations: Scenarios, criteria, and problems of prediction. Physics of Fluids 29(9), 094101 (2017)
Schrader, L. U. (2008). Receptivity of boundary layers under pressure gradient. PhD dissertation, KTH
Goldstein, M.E.: The evolution of Tollmien-Sclichting waves near a leading edge. Journal of Fluid Mechanics, Cambridge University Press 127, 59–81 (1983)
Goldstein, M.E.: Scattering of acoustic waves into Tollmien-Schlichting waves by small streamwise variations in surface geometry. Journal of Fluid Mechanics, Cambridge University Press 154, 509–529 (1985)
Hanson, R.E., Buckley, H.P., Lavoie, P.: Aerodynamic optimization of the flat-plate leading edge for experimental studies of laminar and transitional boundary layers. Experiments in fluids, Springer 53, 863–871 (2012)
N. A. V. Piercy, E. G. Richardson, XCVI-The variation of velocity amplitude close to the surface of a cylinder moving through a viscous fluid, The London, Edinburgh, and Dublin Philosophical Magazine and Journal of Science, vol. 6-39, 970-977, Taylor & Francis (1928)
N. A. V. Piercy, E. G. Richardson, XCIV - The turbulence in front of a body moving through a viscous fluid, The London, Edinburgh and Dublin Philosophical Magazine and Journal of Science, vol. 9-60, 1038-1041, Taylor & Francis (1930)
S. P. Sutera, P. F. Maeder, J. Kesting, On the sensitivity of heat transfer in the stagnation point boundary layer to free stream vorticity, Cambridge Univ Press (1962)
S. P. Sutera, Vorticity amplification in stagnation-point flow and its effect on heat transfer, Journal of Fluid Mechanics, vol. 21-03, 513–534, Cambridge Univ Press (1965)
Sadeh, W.Z., Brauer, H.J., Garrison, J.A.: Visualization Study of Vorticity Amplification in Stagnation Flow. Purdue Univ Lafayette Ind Project Squid (1977). Headquarters
Sadeh, W.Z., Sutera, S.P., Maeder, P.F.: An investigation of vorticity amplification in stagnation flow. Zeitschrift für angewandte Mathematik und Physik ZAMP, Springer 21, 177–742 (1970)
I. Fumarola, Effect of Freestream Turbulence on the Boundary Layer on a Swept Leading Edge. PhD Dissertation, City University of London (2019)
I. Fumarola, M. Gaster, C. Atkin (2019) Enhancement of the velocity fluctuations ahead of the stagnation region of a cylinder (under review)
Pfenninger, W., Bacon, J.W.: Amplified laminar boundary layer oscillations and transition at the front attachment line of a 45 swept flat-nosed wing with and without boundary layer suction, pp. 85–105. Plenum Press, Viscous Drag Reduction proceedings (1969)
Anscombe, A., Illingworth, L.N.: Wind-tunnel Observations of Boundary Layer Transition on a Wing at Various Angles of Sweepback. Aeronautical Research Council Great Britain, HM Stationery Office (1956)
Gaster, M.: On the flow along swept leading edges. The Aeronautical Quarterly, Cambridge University Press 18, 165–184 (1967)
Poll, D. I. A. (1978). Some aspects of the flow near a swept attachment line with particular reference to boundary layer transition. PhD thesis,Cranfield Institute of Technology, College of Aeronautics
Spalart, P. R. (1988). Direct Numerical Study of Leading Edge Contamination. AGARD-CP, 438
Hall, P., Malik, M.R.: On the instability of a three-dimensional attachment-line boundary layer: weakly nonlinear theory and a numerical approach. Journal of Fluid Mechanics, Cambridge University Press 163, 257–282 (1986)
Arnal, D., Casalis, G.: Laminar-turbulent transition prediction in three-dimensional flows. Progress in Aerospace Sciences, Elsevier 36, 173–191 (2000)
Gowree, E. R. Influence of Attachment Line Flow on Form Drag. PhD Dissertation, City University of London (2014)
Gaster, M., Roberts, J.B.: The spectral analysis of randomly sampled records by a direct transform. Proceedings of the Royal Society of London A: Mathematical, Physical and Engineering Sciences, The Royal Society 354, 27–85 (1977)
Acknowledgements
The authors would like to acknowledge the financial support of the Engineering and Physical Sciences Research Council under grant ref. EP L024888 1 UK National Wind Tunnel Facility, co-ordinated by Imperial College, and the support of InnovateUK under grant ref. 113024, Enhanced Fidelity Transonic Wing, led by Airbus.
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Fumarola, I., Gaster, M., Atkin, C.J. (2022). On the Interaction of Freestream Turbulence and Attachment-Line Boundary Layer. In: Sherwin, S., Schmid, P., Wu, X. (eds) IUTAM Laminar-Turbulent Transition. IUTAM Bookseries, vol 38. Springer, Cham. https://doi.org/10.1007/978-3-030-67902-6_15
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DOI: https://doi.org/10.1007/978-3-030-67902-6_15
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