Anderson, J. S., Jungowski, W. M., Hiller, W. J. & Meier, G. E. A.,“Flow oscillations in a duct with a rectangular cross-section” J. Fluid Mech., Vol. 79, No. 4, 1977, pp. 769-784. CrossRef
	Bailly, C., Lafon, P. & Candel, S., “Prediction of supersonic jet noise from a statistical acoustic model and a compressible turbulence closure”, J. Sound Vib., Vol. 194, No. 2, 1996, pp. 219-242. CrossRef
	Bailly, C., Lafon, P. & Candel, S., “Subsonic and supersonic jet noise predictions from statistical source models”, AIAA Journal, Vol. 35, No. 11, 1997, pp. 1688-1696. CrossRef
	Bailly, C. & Bogey, C., “Contributions of computational aeroacoustics to jet noise research and prediction”, International Journal of Computational Fluid Dynamics, Vol. 18, No. 6, 2004, pp. 481-491. CrossRef
	Berland, J., Bogey, C. and Bailly, C., “Low-dissipation and low-dispersion fourth-order Runge-Kutta algorithm”, Computer & Fluids, Vol. 35, No. 10, 2006, pp. 1459-1463.
	Berland, J., Bogey, C. and Bailly, C., “Numerical study of screech generation in a planar supersonic jet”, Phys. Fluids, Vol. 19, 075105, 2007, pp. 1-14. CrossRef
	Berland, J., Bogey, C. and Bailly, C., “Investigation using statistical closure theory of the influence of the filter shape on scale separation in large-eddy-simulation”, Journal Of Turbulence, http://jot.iop.org/, Vol. 9, No. 21, 2008, pp. 1-22. http://jot.iop.org/
	Bogey, C. and Bailly, C., “Investigation of downstream and sideline subsonic jet noise using Large Eddy Simulations”, Theoretical and Computational Fluid Dynamics, Vol. 20, No. 1, 2006, pp. 23-40. CrossRef
	Bogey, C. and Bailly, C., “Large Eddy Simulations of transitional round jets: influence of the Reynolds number on flow development and energy dissipation”, Physics of Fluids, Vol. 18, 065101, 2006, pp. 1-14. CrossRef
	Bogey, C. and Bailly, C., “An analysis of the correlations between the turbulent flow and the sound pressure field of subsonic jets”, Journal of Fluid Mechanics, Vol. 583, 2007, pp. 71-97. CrossRef
	Bogey, C., De Cacqueray, N. and Bailly, C., “A shock-capturing methodology based on adaptative spatial filtering for high-order nonlinear computations”, Journal of Computational Physics, Vol. 228, No. 5, 2009, pp. 1447-1465. CrossRef
	Bui, T. P., Schröder, W. & Meinke, M., “Acoustic perturbation equations for reacting flows to compute combustion noise”, Aeroacoustics, Vol. 6, No.4, 2007, pp. 335-355. Abstract
	Cattafesta III, L. N., Williams, D., Rowley, C. and Alvi, F., “Review of active control of flow-induced cavity resonance”, AIAA Paper 2003-3567.
	Colonius, T. (2001), An overview of simulation, modeling and active control of flow/acoustic resonance in open cavities, AIAA Paper 2001-0076, pp. 1-12.
	Colonius, T., “Modeling artificial boundary conditions for compressible flows”, Annu. Rev. Fluid Mech., Vol. 36, 2004, pp. 315-345. CrossRef
	Colonius, T. and Lele, S., “Computational aeroacoustics: progress on nonlinear problems on sound generation”, Progress in Aerospace Sciences, Vol. 40, 2004, pp. 345-416. CrossRef
	Curle, N., “The influence of solid boundaries on aerodynamic sound”, Proc. Roy. Soc. London, Vol. A231, No. 1187, 1955, pp. 505-514.
	Domaradzki, J. A. & Adams, N. A, “Direct modelling of subgrid scales of turbulence in large eddy simulations”, Journal Of Turbulence, http://jot.iop.org/, Vol. 3, No. 024, 2002, pp. 10-19. http://jot.iop.org
	Emmert, T., Lafon, P. and Bailly, C., “Numerical study of self-induced transonic flow oscillations behind a sudden duct enlargement”, Phys. Fluids, Vol. 21, 2009.
	Ffowcs Williams, J. E. and Hawkings, D. L., Sound generation by turbulence and surfaces in arbitrary motion, Phil. Trans. Roy. Soc. London, Vol. 264, Ser. A, 1151, 1969, pp. 321-342.
	Freund, J.B., “Noise sources in a low-Reynolds-number turbulent jet at Mach 0.9”, J. Fluid Mech., Vol. 438, 2001, pp. 277-305.
	Gloerfelt, X., Pérot, F., Bailly, C. and Juvé, D., “Flow-induced cylinder noise formulated as diffraction problem for low Mach number flows”, J. Sound Vib., Vol. 287, No. 1-2, 2005, pp. 129-151. CrossRef
	Gloerfelt, X., Bogey, C. and Bailly, C., “Numerical evidence of mode switching in the flow-induced oscillations by a cavity”, International Journal of Aeroacoustics, Vol. 2, No. 2, 2003, pp. 193-217. Abstract
	Goldstein, M. E., “An exact form of Lilley's equation with a velocity quadrupole/temperature dipole source term”, J. Fluid Mech., Vol. 443, 2001, pp. 231-236.
	Krothapalli, A., Hsia, Y., Baganoff, D. and Karamcheti, K., “The role of screech tones in mixing of an underexpanded rectangular jet”, J. Sound Vib., Vol. 106, No. 1, 1986, pp. 119-143. CrossRef
	Lighthill, M.J., “On sound generated aerodynamically - I. General theory”, Proc. Roy. Soc. London, Vol. 211, Ser. A, 1107, 1952, pp. 564-587. CrossRef
	Lilley, G. M., “On the noise from air jets”, British Aeronautical Research Council, A.R.C. 20-276, 1958.
	Marsden, O., Gloerfelt, X. and Bailly, C., “Direct noise computation of adaptive control applied to a cavity flow”, C. R. Méc., Acad. Sci. Paris, Vol. 331, No. 6, 2003, pp. 423-429.
	Marsden, O., Bogey, C. and Bailly, C., “Direct noise computation of the turbulent flow around a zero-incidence airfoil”, AIAA Journal, Vol. 46, No. 4, pp. 874-883.
	Meier, G.E.A., Grabitz, G., Jungowski, W.M., Witczak, K.J. and Anderson, J.S. (1978) Oscillations of the supersonic flow downstream of an abrupt increase in duct cross-section, Mitteilung aus dem Max-Plancklnstitut fuer Stroemungsforschung und der Aerodynamischen Versuchsanstalt, Göttingen, Vol. 65.
	Meier, G.E.A., Szumowski, A.P. and Selerowicz, W.C., “Self-excited oscillations in internal transonic flows”, Prog. Aerospace Sci., Vol. 27, 1990, pp. 145-200. CrossRef
	Möhring, W., Müller, E.-A. & Obermeier, F., “Problems in flow acoustics”, Rev. Mod. Phys., Vol. 55, No. 3, 1983, pp. 707-724. CrossRef
	Morris, P. J. & Farassat, F., “Acoustic analogy and alternative theories for jet noise predictions”, AIAA Journal, Vol. 40, No. 4, 2002, pp. 671-680. CrossRef
	Oberai, A. A., Ronaldki, F. and Hughes, T. J. R. (2000), Computational procedures for determining structural-acoustic response due to hydrodynamic source, Comput. Methods Appl. Mech. Engrg., Vol. 190, pp. 345-361. CrossRef
	M. Omais, B. Caruelle, S. Redonnet, E. Manoha, P. Sagaut, “Jet Noise Prediction Using RANS CFD Input”, AlAA-Paper 2008-2938.
	Piellard, M., and Bailly, C. (2008), Validation of a hybrid CAA method and application to the case of a diaphragm in a duct at low Mach number, 14th AIAA/CEAS Aeroacoustics Conference, Paper 2008-2873.
	Powell, A., “The influence of the exit velocity profile on the noise of a jet”, Aeronautical Quaterly, Vol. 4, 1953, pp. 341-360.
	Prax, C., Golanski, F. & Nadal, N., “Control of the vorticity mode in the linearized Euler equations for hybrid aeroacoustic prediction”, J. Comput. Phys., Vol. 277, 2008, pp. 6044-6057.
	Raman, G., “Supersonic jet screech: half-century from Powell to the present”, J. Sound Vib., Vol. 225, No. 3, 1999, pp. 543-571. CrossRef
	Rowley, C.W. and Williams, D.R., “Dynamics and control of high-Reynolds-number flow over open cavities”, Annu. Rev. Fluid Mech., Vol. 38, 2006, pp. 251-276. CrossRef
	Shen, H. and Tam, C. K. W., “Effects of jet temperature and nozzle-lip thickness on screech tones”, AIAA Journal, Vol. 38, No. 5, 2000, pp. 762-767. CrossRef
	Sherer, S. E. and Scott, J. N., “High-order compact finite-difference methods on general overset grids”, J. Comput. Phys., Vol. 210, 2005, pp. 459-496. CrossRef
	Suzuki, T. and Lele, S., “Shock leakage through an unsteady vortex-laden mixing layer: application to screech jet”, Journal Fluid Mech., Vol. 490, 2003, pp. 139-167. CrossRef
	Tam, C.K.W., “The shock-cell structures and screech tone frequencies of rectangular and non-axisymmetric supersonic jets”, J. Sound Vib., Vol. 121, No. 1, 1988, pp. 135-147. CrossRef
	Tam, C.K.W. (1995) Supersonic jet noise, Annu. Rev. Fluid Mech., Vol. 27, pp. 17-43. CrossRef
	Tam, C.K.W., Seiner, J.M. and Yu, J.C., “Proposed relationship between broadband shock associated noise and screech tones”, J. Sound Vib., Vol. 110, No. 2, 1986, pp. 309-321. CrossRef
	Tam, C. K. W., Viswanathan, K., Ahuja, K. K. and Panda, J., “The sources of jet noise: experimental evidence”, J. Fluid Mech., Vol. 615, 2008, pp. 253-292. CrossRef
	Utzmann, J., Schwartzkopff, T., Dumbser, M. & Munz, C.-D., “Heterogeneous domain decomposition for computational aeroacoustics”, AIAA Journal, Vol. 44, No. 10, 2006, pp. 2231-2250. CrossRef
	Visbal, M. R. & Gordnier, R. E., 2004, “Numerical simulation of the interaction of a transitional boundary layer with a 2-D flexible panel in the subsonic regime”, Journal Fluids Struct., Vol. 19, No. 7, 2004, pp. 881-903. CrossRef
	Wang, M., Freund, J.B. and Lele, S.K., “Computational prediction of flow-generated sound”, Annu. Rev. Fluid Mech., Vol. 38, 2006, pp. 483-512. CrossRef
	Xu, S. and Martin, M. P., “Assessment of inflow boundary conditions for compressible turbulent boundary layers”, Phys. Fluids, Vol. 16, No. 7, 2004, pp. 2623-2639. CrossRef
	Zaman, K. B. M. Q., “Effect of initial condition on subsonic jet noise”, AIAA Journal, Vol. 23, No. 9, 1985, pp. 1370-1373. CrossRef
	Bogey, C. and Bailly, C., “Turbulence and energy budget in a self-preserving round jet: direct evaluation using large-eddy simulation”, J. Fluid Mech., Vol. 627, 2009, pp. 129-160 CrossRef
	Bogey, C. and Bailly, C., “Influence of the nozzle-exit boundary-layer thickness on the flow and acoustic fields of initially laminar jets”, 15th AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2009-3409.