The long-time impulse response of compressible swept-wing boundary layers

Journal of Fluid Mechanics

Volumn 379, Issue , 1999, Pages 333-350

  Taylor, M J ^a   Peake, N ^a  

^a UNIVERSITY OF CAMBRIDGE   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; INCOMPRESSIBLE FLOW; SUBSONIC FLOW; SUPERSONIC FLOW; WIND TUNNELS; WINGS;

FALKER-SKAN-COOKE PROFILES; MODAL PINCH POINTS;

BOUNDARY LAYERS;

EID: 0032688995     PISSN: 00221120     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0022112098003516     Document Type: Article

References (26)

1. BERS, A. 1975 Linear waves and instabilities In Physique des Plasmas (ed. C. DeWitt & J. Peyraud), pp. 113-215. Gordon and Breach.
2. BREVDO, L. 1991 Three-dimensional absolute and convective instabilities, and spatially amplifying waves in parallel shear flows. Z. Angew. Math. Phys. 42, 911-942.
3. BRIGGS, R. 1964 Electron-Stream Interaction with Plasmas. MIT Press.
4. CEBECI, T. & STEWARTSON, K. 1979 On the prediction of transition in three-dimensional flows. In Laminar-Turbulent Transition (ed. R. Eppler & H. Fasel), pp. 243-252. Springer.
5. GASTER, M. 1962 A note on the relation between temporally-increasing and spatially-increasing disturbances in hydrodynamic stability. J. Fluid Mech. 14, 222-224.
6. GASTER, M. 1967 On the flow along swept leading edges. Aeronaut. Q. 18, 165-184.
7. GREGORY, N. 1960 Transition and the spread of turbulence on a 60° swept-back wing. J. R. Aero. Soc. 64, 562-564.
8. HALL, P., MALIK, M. & POLL, D. 1984 On the stability of the infinite swept attachment line boundary layer. Proc. R. Soc. Lond. A 395, 229-245.
9. KAUPS, K. & CEBECI, T. 1977 Compressible laminar boundary layers with suction on swept and tapered wings. J. Aircraft 14, 661-667.
10. KUPFER, K., BERS, A. & RAM, A. 1987 The cusp map in the complex-frequency plane for absolute instabilities. Phys. Fluids 30, 3075-3082.
11. LIN, R. & MALIK, M. 1996 On the stability of attachment-line boundary layers. Part 1. The incompressible swept Hiemenz flow. J. Fluid Mech. 311, 239-255.
12. LINGWOOD, R. 1997 On the impulse response for swept boundary layer flows. J. Fluid Mech. 344, 317-334.
13. MACK, L. 1984 Special course on stability and transition of laminar flow. AGARD Rep. 709. NATO.
14. MALIK, M. 1990 Numerical methods for hypersonic boundary layer stability. Comput. Phys. 86, 376-413.
15. MALIK, M. & ORSZAG, S. 1980 Comparison of methods for prediction of transition by stability analysis. AIAA J. 18 1485-1489.
16. MALIK, M. & ORSZAG, S. 1981 Efficient computation of the stability of three-dimensional compressible boundary layers. AIAA Paper 81-1277.
17. NAYFEH, A. 1979 Stability of three-dimensional boundary layers. AIAA Paper 79-0262.
18. PFENNINGER, W. 1965 Flow phenomena at the leading edge of swept wings. AGARDograph 97 Part IV A1. NATO.
19. RADKEY, R., WELGE, H. & FELIX, J. 1977 Aerodynamic characteristics of a Mach 2.2 advanced supersonic cruise aircraft configuration at Mach numbers from 0.5 to 2.4. Contractors Report CR-145094. NASA.
20. RYZHOV, O. S., COLE, J. D. & MALMATH, N. D. 1998 Excitation of convectively and absolutely unstable disturbances in three-dimensional boundary layers. AIAA Paper 98-2861.
21. RYZHOV, O. S. & TERENT'EV, E. D. 1998 Streamwise absolute instability of a three-dimensional boundary layer at high Reynolds number. J. Fluid Mech. 373, 111-153.
22. SCHRAUF, G. 1994 Transition prediction using different linear stability analysis strategies. AIAA Paper 94-1848.
23. SMITH, A. & GAMBERONI, N. 1956 Transition, pressure gradient and stability theory. Rep. ES 26388. Douglas Aircraft Co.
24. TAYLOR, M. 1997 The stability of the boundary layer on swept wings. PhD thesis, University of Cambridge.
25. TAYLOR, M. & PEAKE, N. 1998 The long-time behaviour of incompressible swept wing boundary layers subject to impulsive forcing, J. Fluid Mech. 355, 359-381 (referred to herein as TP).
26. VAN INGEN, J. 1956 A suggested semi-empirical method for the calculation of the boundary layer transition region. Rep. VTH-74. Univ. of Tech, Delft.