Global stability of swept flow around a parabolic body: Connecting attachment-line and crossflow modes

Journal of Fluid Mechanics

Volumn 611, Issue , 2008, Pages 205-214

  Mack, Christoph J ^a   Schmid, Peter J ^b   Sesterhenn, Jörn L ^a  

^a BUNDESWEHR UNIVERSITY MUNICH   (Germany)

^b ECOLE POLYTECHNIQUE   (France)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; BOUNDARY LAYERS; ITERATIVE METHODS; NUMERICAL METHODS; VORTEX FLOW;

AMPLITUDE DISTRIBUTIONS; ATTACHMENT LINES; CROSSFLOW VORTICES; EIGENVALUE METHODS; GLOBAL STABILITY; INSTABILITY MECHANISMS; PARAMETER STUDIES; THREE-DIMENSIONAL BOUNDARY LAYERS;

EIGENVALUES AND EIGENFUNCTIONS;

COMPRESSIBLE FLOW; EIGENVALUE; FLOW AROUND OBJECT; FLOW STABILITY; NUMERICAL MODEL; THREE-DIMENSIONAL FLOW;

EID: 50949104249     PISSN: 00221120     EISSN: 14697645     Source Type: Journal    
DOI: 10.1017/S0022112008002851     Document Type: Article

References (19)

1. BERTOLOTTI, F. P. 1999 On the connection between cross-flow vortices and attachment-line instabilities. in IUTAM Symp. on Laminar-Turbulent Transition, pp. 625-630. Sedona, USA.
2. BIPPES, H. 1999 Basic experiments on transition in three-dimenional boundary layers dominated by crossflow instability. Prog. Aero. Sci. 35, 363-412.
3. EDWARDS, W. S., TUCKERMAN, L. S., FRIESNER, R. A. & SORENSEN, D. C. 1994 Krylov methods for the incompressible Navier Stokes equations. J. Comput. Phys. 110, 82-102.
4. FABRE, D., JACQUIN, L. & SESTERHENN, J. 2001 Linear interaction of a cylindrical entropy spot with a shock. Phys. Fluids 13 (8), 2403-2422.
5. GRAY, W. E. 1952 The effect of wing sweep on laminar flow. Tech. Rep. RAE TM Aero 255. British Royal Aircraft Establishment.
6. GUÉGAN, A., SCHMID, P. J. & HUERRE, P. 2006 Optimal energy growth and optimal control in swept Hiemenz flow. J. Fluid Mech. 566, 11-45.
7. HALL, P., MALIK, M. & POLL, D. I. A. 1984 On the stability of an infinite swept attachment-line boundary layer. Proc. R. Soc. Lord. A 395, 229-245.
8. HERBERT, T. 1997 Parabolized stability equations. Annu. Rev. Fluid Mech. 29, 245-283.
9. JOSLIN, R. D. 1995 Direct simulation of evolution and control of three-dimensional instabilities in attachment-line boundary layers. J. Fluid Mech. 291, 369-392.
10. LE DUC, A., SESTERHENN, J & FRIEDRICH, R. 2006 Instabilities in compressible attachment-line boundary layers. Phys. Fluids 18 044102.
11. LIN, R. S. & MALIK, M. R. 1995 Stability and transition in compressible attachment-line boundary-layer flow. Tech. Rep. 95204. SAE.
12. LIN, R. S. & MALIK, M. R. 1996 On the stability of attachment-line boundary layers. Part 1. The incompressible swept Hiemenz flow. J. Fluid Mech. 311, 239-255.
13. LIN, R. S. & MALIK, M. R. 1997 On the stability of attachment-line boundary layers. Part 2. The effect of leading edge curvature. J. Fluid Mech. 333, 125-137.
14. OSWATITSCH, K. 1956 Gas Dynamics. Academic.
15. POLL, D. I. A. 1979 Transition in the infinite swept attachment-line boundary layer. Aero. Q. 30, 607-628.
16. REED, H. L. & SARIC, W. S. 1989 Stability of three-dimensional boundary layers. Annu. Rev. Fluid Mech. 21, 235-284.
17. SARIC, W. S., REED, H. L. & WHITE, E. B. 2003 Stability and transition of three-dimensional boundary layers. Annu. Rev. Fluid Mech. 35, 413-440.
18. SESTERHENN, J. 2001 A characteristic-type formulation of the Navier-Stokes equations for high-order upwind schemes. Comput. Fluids 30, 37-67.
19. SPALLART, P. R. 1988 Direct numerical study of leading-edge contamination. In AGARD-CP-438, pp. 5/1-5/13.