On the stability of attachment-line boundary layers. Part 1. The incompressible swept Hiemenz flow

Journal of Fluid Mechanics

Volumn 311, Issue , 1996, Pages 239-255

  Lin, Ray Sing ^a   Malik, Mujeeb R ^a  

^a High Technology Corporation   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPRESSIBILITY; EIGENVALUES AND EIGENFUNCTIONS; LAMINAR FLOW; NAVIER STOKES EQUATIONS; PARTIAL DIFFERENTIAL EQUATIONS; PERTURBATION TECHNIQUES; PROBLEM SOLVING; STABILITY;

ATTACHMENT LINE BOUNDARY LAYERS; DISTURBANCE FIELD; INCOMPRESSIBLE SWEPT HIEMENS FLOW; SPANWISE WAVENUMBER TRAVEL;

BOUNDARY LAYER FLOW;

BOUNDARY LAYERS; FLOW STABILITY; INCOMPRESSIBLE FLOW; NAVIER-STOKES EQUATIONS;

EID: 0029671719     PISSN: 00221120     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0022112096002583     Document Type: Article

References (22)

1. ARNAL, D. & JUILLEN, J. C. 1989 Leading edge contamination and relaminarization on a swept wing at incidence. 4th Symp. on Numerical and Physical Aspects of Aerodynamic flows (ed. T. Cebeci). Springer.
2. CANUTO, C., HUSSAINI, M. Y., QUARTERONI, A. & ZANG, T. A. 1987 Spectral Methods in Fluid Mechanics, Springer.
3. GASTER, M. 1967 On the flow along swept leading edges. Aero. Q. 18, 165-184.
4. GRAY, W. E. 1952 The effect of wing sweep on laminar flow. RAE TM 255. Royal Aircraft Establishment, Farnborough, UK.
5. GÖRTLER, H. 1955 Dreidimensionale Instabilität der ebenen Staupunkt-Strömung gegenüber wirbelartigen Störungen. In Fifty Years of Boundary Layer Research (ed. H. Görtler & W. Tollmien), p. 304. Vieweg und Sohn.
6. 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, 257-282.
7. 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, 229-245.
8. HALL, P. & SEDDOUGUI, S. O. 1990 Wave interactions in a three-dimensional attachment-line boundary layer. J. Fluid Mech. 217, 367-390.
9. HÄMMERLIN, G. 1955 Zur Instabilitätstheorie der ebenen Staupunkströmung. In Fifty Years of Boundary Layer Research (ed. H. Görtler & W. Tollmien), p. 315. Vieweg und Sohn.
10. JUILLEN, J. C. & ARNAL, D. 1995 Experimental study of boundary layer suction effects on leading edge contamination along the attachment line of a swept wing. Laminar-Turbulent Transition (ed. R. Kobayashi), p. 173. Springer.
11. LANDAU, L. D. 1944 On the problem of turbulence. C.R. Acad. Sci. URSS 44, 311-314.
12. MALIK, M. R., ZANG, T. A. & HUSSAINI, M. Y. 1985 A spectral collocation method for the Navier-Stokes equation. J. Comput. Phys. 61, 64-88.
13. ORSZAG, S. A. 1971 Accurate solution of the Orr-Sommerfeld stability equation. J. Fluid Mech. 50, 689-703.
14. PFENNINGER, W. 1965 Flow phenomena at the leading edge of swept wings. Recent developments in boundary layer research-Part IV. AGARDograph 97, May 1965.
15. PFENNINGER, W. & BACON, J. W. 1969 Amplified laminar boundary layer oscillations and transition at the front attachment line of a 45° flat-nosed wing with and without boundary layer suction. In Viscous Drag Reduction (ed. C. S. Wells). Plenum.
16. POLL, D. I. A. 1978 Some aspects of the flow near a swept attachment line with particular reference to boundary layer transition. College of Aeronautics Rep. 7805.
17. POLL, D. I. A. 1979 Transition in the infinite swept attachment line boundary layer. Aero. Q. 30, 607.
18. POLL. D. I. A. & DANKS, M. 1995 Relaminarisation of the swept wing attachment-line by surface suction. Laminar-Turbulent Transition (ed. R. Kobayashi), p. 137. Springer.
19. ROSENHEAD, L. 1963 Laminar Boundary Layers, pp. 467-75. Oxford University Press.
20. SPALART, P. R. 1988 Direct numerical study of leading edge contamination. AGARD CP 438.
21. WILKISON, J. 1965 The Algebraic Eigenvalue Problem. Oxford University Press.
22. WILSON, S. D. R. & GLADWELL, I. 1978 The stability of a two-dimensional stagnation flow to three-dimensional disturbances. J. Fluid Mech. 84, 517-527.