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Global stability of swept flow around a parabolic body: the neutral curve

Published online by Cambridge University Press:  12 May 2011

CHRISTOPH J. MACK
Affiliation:
Laboratoire d'Hydrodynamique (LadHyX), CNRS-École Polytechnique, F-91128 Palaiseau, France Department of Numerical Mathematics, Universität der Bundeswehr (UniBw), D-85577 Munich, Germany
PETER J. SCHMID*
Affiliation:
Laboratoire d'Hydrodynamique (LadHyX), CNRS-École Polytechnique, F-91128 Palaiseau, France
*
Email address for correspondence: [email protected]

Abstract

The onset of transition in the leading-edge region of a swept blunt body depends crucially on the stability characteristics of the flow. Modelling this flow configuration by swept compressible flow around a parabolic body, a global approach is taken to extract pertinent stability information via a DNS-based iterative eigenvalue solver. Global modes combining features from boundary-layer and acoustic instabilities are presented. A parameter study, varying the spanwise disturbance wavenumber and the sweep Reynolds number, showed the existence of unstable boundary-layer and acoustic modes. The corresponding neutral curve displays two overlapping regions of exponential growth and two critical Reynolds numbers, one for boundary-layer instabilities and one for acoustic instabilities. The employed global approach establishes a first neutral curve, delineating stable from unstable parameter configurations, for the complex flow about a swept parabolic body with corresponding implications for swept leading-edge flow.

Type
Papers
Copyright
Copyright © Cambridge University Press 2011

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References

REFERENCES

Gaillard, L., Benard, E. & Alziary de Roquefort, T. 1999 Smooth leading-edge transition in hypersonic flow. Exp. Fluids 26, 169176.CrossRefGoogle Scholar
Gaster, M. 1965 A simple device for preventing turbulent contamination on swept leading edges. J. R. Aeronaut. Soc. 69 (659), 788789.CrossRefGoogle Scholar
Gaster, M. 1967 On the flow along swept leading edges. Aeronaut. Q. 18 (2), 165184.CrossRefGoogle Scholar
Gray, W. E. 1952 The effect of wing sweep on laminar flow. Tech. Rep. RAE TM Aero 255. British Royal Aircraft Establishment.Google Scholar
Hall, P. & Malik, M. 1986 On the instability of a three-dimensional attachment-line boundary layer: weakly nonlinear theory and a numerical approach. J. Fluid Mech. 163, 257282.CrossRefGoogle Scholar
Hall, P., Malik, M. & Poll, D. I. A. 1984 On the stability of an infinite swept attachment-line boundary layer. Proc. R. Soc. Lond. A 395, 229245.Google Scholar
Joslin, R. D. 1995 Direct simulation of evolution and control of three-dimensional instabilities in attachment-line boundary layers. J. Fluid Mech. 291, 369392.CrossRefGoogle Scholar
Joslin, R. D. 1996 Simulation of three-dimensional symmetric and asymmetric instabilities in attachment-line boundary layers. AIAA J. 34 (11), 24322434.CrossRefGoogle Scholar
Lehoucq, R. B., Sorensen, D. C. & Yang, C. 1998 ARPACK Users' Guide: Solution of Large-Scale Eigenvalue Problems with Implicitly Restarted Arnoldi Methods. SIAM.CrossRefGoogle Scholar
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, 239255.CrossRefGoogle Scholar
Mack, C. J. & Schmid, P. J. 2010 a Direct numerical study of hypersonic flow about a swept parabolic body. Comput. Fluids 39, 19321943.CrossRefGoogle Scholar
Mack, C. J. & Schmid, P. J. 2010 b A preconditioned Krylov technique for global hydrodynamic stability analysis of large-scale compressible flows. J. Comput. Phys. 229 (3), 541560.CrossRefGoogle Scholar
Mack, C. J. & Schmid, P. J. 2011 Global stability of swept flow around a parabolic body: features of the global spectrum. J. Fluid Mech. 669, 375396.CrossRefGoogle Scholar
Mack, C. J., Schmid, P. J. & Sesterhenn, J. S. 2008 Global stability of swept flow around a parabolic body: connecting attachment-line and crossflow modes. J. Fluid Mech. 611, 205214.CrossRefGoogle Scholar
Pfenninger, W. 1965 Some results from the X-21 program. Part I. Flow phenomena at the leading edge of swept wings. Tech. Rep. 97. AGARDograph.Google Scholar
Poll, D. I. A. 1979 Transition in the infinite swept attachment-line boundary layer. Aeronaut. Q. 30, 607628.CrossRefGoogle Scholar
Poll, D. I. A. 1983 The development of intermittent turbulence on a swept attachment line including the effects of compressibility. Aeronaut. Q. 34, 123.CrossRefGoogle Scholar
Poll, D. I. A. 1984 Transition description and prediction in three-dimensional flows. In Special Course on Stability and Transition of Laminar Flow, pp. 5/1–5/23. AGARD.Google Scholar
Semisynov, A. I., Fedorov, A. V., Novikov, V. E., Semionov, N. V. & Kosinov, A. D. 2003 Stability and transition on a swept cylinder in a supersonic flow. J. Appl. Mech. Tech. Phys. 44, 212220.CrossRefGoogle Scholar
Spalart, P. R. 1988 Direct numerical study of leading-edge contamination. In AGARD-CP-438, pp. 5/1–5/13.Google Scholar