Hostname: page-component-cd9895bd7-dzt6s Total loading time: 0 Render date: 2024-12-19T06:40:48.715Z Has data issue: false hasContentIssue false

Wave interactions in a three-dimensional attachment-line boundary layer

Published online by Cambridge University Press:  26 April 2006

Philip Hall
Affiliation:
Department of Mathematics, Exeter University, North Park Road, Exeter, Devon EX4 4QE, UK
Sharon O. Seddougui
Affiliation:
Institute for Computer Applications in Science and Engineering, NASA Langley Research Centre, Hampton, VA 23665, USA

Abstract

The three-dimensional boundary layer on a swept wing can support different types of hydrodynamic instability. Here attention is focused on the so-called ‘spanwise instability’ problem which occurs when the attachment-line boundary layer on the leading edge becomes unstable to Tollmien–Schlichting waves. In order to gain insight into the interactions that are important in that problem a simplified basic state is considered. This simplified flow corresponds to the swept attachment-line boundary layer on an infinite flat plate. The basic flow here is an exact solution of the Navier–Stokes equations and its stability to two-dimensional waves propagating along the attachment line can be considered exactly at finite Reynolds number. This has been done in the linear and weakly nonlinear regimes by Hall, Malik & Poll (1984) and Hall & Malik (1986). Here the corresponding problem is studied for oblique waves and their interaction with two-dimensional waves is investigated. In fact oblique modes cannot be described exactly at finite Reynolds number so it is necessary to make a high-Reynolds-number approximation and use triple-deck theory. It is shown that there are two types of oblique wave which, if excited, cause the destabilization of the two-dimensional mode and the breakdown of the disturbed flow at a finite distance from the leading edge. First a low-frequency mode closely related to the viscous stationary crossflow mode discussed by Hall (1986) and MacKerrell (1987) is a possible cause of breakdown. Secondly a class of oblique wave with frequency comparable with that of the two-dimensional mode is another cause of breakdown. It is shown that the relative importance of the modes depends on the distance from the attachment line.

Type
Research Article
Copyright
© 1990 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

Bassom, A. P. & Gajjar, J. S. B. 1988 Non-stationary cross-flow vortices in three-dimensional boundary-layer flows. Proc. R. Soc. Lond. A 417, 179212.Google Scholar
Bassom, A. P. & Hall, P. 1990 On the interaction of crossflow vortices and Tollmien—Schlichting waves in the boundary layer on a rotating disc. Proc. R. Soc. Lond. A 430, 2555.Google Scholar
Gaster, M. 1967 On the flow along swept leading edges. Aero. Q. 18, 165184.Google Scholar
Gregory, N., Stuart, J. T. & Walker, W. S. 1955 On the stability of three-dimensional boundary layers with application to the flow due to a rotating disc. Phil. Trans. R. Soc. Lond. A 248, 155199.Google Scholar
Hall, P. 1986 An asymptotic investigation of the stationary modes of instability of the boundary layer on a rotating disc. Proc. R. Soc. Lond. A 406, 93106.Google Scholar
Hall, P. & Malik, M. R. 1986 On the instability of a three-dimensional attachment-line boundary layer: weakly nonlinear theory and a numerical approach. J. Fluid Mech. 163, 257282 (referred to herein as HM).Google Scholar
Hall, P., Malik, M. R. & Poll, D. I. A. 1984 On the stability of an infinite swept attachment line boundary layer. Proc. R. Soc. Lond. A 395, 229245 (referred to herein as HMP).Google Scholar
Hall, P. & Smith, F. T. 1984 On the effects of nonparallelism, three-dimensionality, and mode interaction in nonlinear boundary-layer stability. Stud. Appl. Maths 70, 91120.Google Scholar
MacKerrell, S. O. 1987 A nonlinear, asymptotic investigation of the stationary modes of instability of the three-dimensional boundary layer on a rotating disc. Proc. R. Soc. Lond. A 413, 497513.Google Scholar
Pfenninger, W. & Bacon, J. W. 1969 Viscous Drag Reduction (ed. C. S. Wells), pp. 85255. Plenum.
Poll, D. I. A. 1979 Transition in the infinite swept attachment line boundary layer. Aero. Q. 30, 607629.Google Scholar
Smith, F. T. 1979a On the non-parallel flow stability of the Blasius boundary layer. Proc. R. Soc. Lond. A 366, 91109.Google Scholar
Smith, F. T. 1979b Nonlinear stability of boundary layers for disturbances of various sizes. Proc. R. Soc. Lond. A 368, 573589.Google Scholar