Fluid-acoustic interactions in self-sustained oscillations in turbulent cavity flows. I. Fluid-dynamic oscillations
Phys. Fluids 21, 105103 (2009); doi:10.1063/1.3253326
Published 23 October 2009
You are not logged in to this journal. Log in
The fluid-acoustic interactions in a flow over a two-dimensional rectangular cavity are investigated by directly solving the compressible Navier–Stokes equations. The upstream boundary layer is turbulent. The depth-to-length ratio of the cavity is 0.5. Phase-averaged flow fields reveal the mechanism for the acoustic radiation. Large-scale vortices form in the shear layer that separates from the upstream edge of the cavity. When a large-scale vortex collides with the downstream wall, the low-pressure fluid in the vortex spreads along the downstream wall. As a result, a local downward velocity is induced by the local pressure gradient, causing the upstream fluid to expand. Finally, an expansion wave propagates to the outside of the cavity. The large-scale vortices originate from the convective disturbances that develop in the shear layer. The disturbances grow due to the Kelvin–Helmholtz instability, similar to the growth of those in a laminar cavity flow. To clarify the mechanism for the generation of the initial convective disturbances, computations for backward-facing step flows with an artificial acoustic source are also performed. As the artificial acoustic waves become more intense, the initial convective disturbances in the shear layer become more intense while the spatial growth rate of these disturbances does not change. This means that the initial convective disturbances in the shear layer are induced by the acoustic waves.
©2009 American Institute of Physics
| History: | Received 25 March 2009; accepted 18 September 2009; published 23 October 2009 |
| Permalink: |
http://link.aip.org/link/?PHFLE6/21/105103/1 |
KEYWORDS and PACS
RELATED DATABASES
PUBLICATION DATA
1070-6631 (print)
1089-7666 (online)
REFERENCES (28)
For access to fully linked references, you need to log in.
For access to fully linked references, you need to Log in.
- K. Karamcheti, “Acoustic radiation from two-dimensional rectangular cutouts in aerodynamic surfaces,” NACA Report No. TN 3487, 1955.
- F. Mizushima, H. Takakura, T. Kurita, C. Kato, and A. Iida, “Experimental investigation of aerodynamic noise generated by a train-car gap,”
J. Fluid Sci. Technol. 2, 464 (2007) . - P. Oshkai and T. Yan, “Experimental investigation of coaxial side branch resonators,”
J. Fluids Struct. 24, 589 (2008) . - J. C. Bruggeman, A. Hirschberg, M. E. H. van Dongen, and A. P. J. Wijnands, “Self-sustained aeroacoustic pulsations in gas transport systems: Experimental study of the influence of closed side branches,”
J. Sound Vib. 150, 371 (1991) . - J. E. Rossiter, “Wind-tunnel experiments on the flow over rectangular cavities at subsonic and transonic speeds,” Aeronautical Research Council Report No. 3438, 1964.
- A. Powell, “On the edge tone,”
J. Acoust. Soc. Am. 33, 395 (1961) . - L. F. East, “Aerodynamically induced resonance in rectangular cavities,”
J. Sound Vib. 3, 277 (1966) . - D. Rockwell and E. Naudascher, “Review—self-sustaining oscillations of flow past cavities,”
ASME Trans. J. Fluids Eng. 100, 152 (1978) . - C. Knisely and D. Rockwell, “Self-sustained low-frequency components in an impinging shear layer,”
J. Fluid Mech. 116, 157 (1982) . - C. W. Rowley, T. Colonius, and A. J. Basu, “On self-sustained oscillations in two-dimensional compressible flow over rectangular cavities,”
J. Fluid Mech. 455, 315 (2002) . - S. K. Lele, “Compact finite difference schemes with spectral-like resolution,”
J. Comput. Phys. 103, 16 (1992) . - D. P. Rizzetta and M. R. Visbal, “Large-eddy simulation of supersonic cavity flow fields including flow control,”
AIAA J. 41, 1452 (2003) . - C. Bogey and C. Bailly, “Large eddy simulations of round free jets using explicit filtering with/without dynamic Smagorinsky model,”
Int. J. Heat Fluid Flow 27, 603 (2006) . - C. Bogey and C. Bailly, “Turbulence and energy budget in a self-preserving round jet: Direct evaluation using large eddy simulation,”
J. Fluid Mech. 627, 129 (2009) . - K. Matsuura and C. Kato, “Large-eddy simulation of compressible transitional flows in a low-pressure turbine cascade,”
AIAA J. 45, 442 (2007) . - D. V. Gaitonde and M. R. Visbal, “Padé-type higher-order boundary filters for the Navier–Stokes equations,”
AIAA J. 38, 2103 (2000) . - K. W. Thompson, “Time dependent boundary conditions for hyperbolic systems,”
J. Comput. Phys. 68, 1 (1987) . - T. J. Poinsot and S. K. Lele, “Boundary conditions for direct simulations of compressible viscous flows,”
J. Comput. Phys. 101, 104 (1992) . - J. W. Kim and D. J. Lee, “Generalized characteristic boundary conditions for computational aeroacoustics,”
AIAA J. 38, 2040 (2000) . - J. B. Freund, “Proposed inflow/outflow boundary condition for direct computation of aerodynamic sound,”
AIAA J. 35, 740 (1997) . - J. Larsson, L. Davidson, M. Olsson, and L. Eriksson, “Aeroacoustic investigation of an open cavity at low Mach number,”
AIAA J. 42, 2462 (2004) . - H. Yokoyama, Y. Tsukamoto, C. Kato, and A. Iida, “Self-sustained oscillations with acoustic feedback in flows over a backward-facing step with a small upstream step,” Phys. Fluids 19, 106104 (2007).
- J. O. Hinze, Turbulence, 2nd ed. (McGraw-Hill, New York, 1975), pp. 175–320.
- J. Coupland, “Transition modeling for turbomachinery flows, T3 test cases,” ERCOFTAC Bulletin, No. 5, 1990.
- S. K. Robinson, “Coherent motions in the turbulent boundary layer,”
Annu. Rev. Fluid Mech. 23, 601 (1991) . - T. L. Jackson and C. E. Grosch, “Inviscid spatial stability of a compressible mixing layer,”
J. Fluid Mech. 208, 609 (1989) . - M. Zhuang, T. Kubota, and P. E. Dimotakis, “Instability of inviscid, compressible free shear layers,”
AIAA J. 28, 1728 (1990) . - C. K. W. Tam and J. C. Hardin, Second Computational Aeroacoustics (CAA) Workshop on Benchmark problems, NASA, CP 3352 (1997).







