Large-eddy simulation of the flow and acoustic fields of a Reynolds number 105 subsonic jet with tripped exit boundary layers

Physics of Fluids

Volumn 23, Issue 3, 2011, Pages

  Bogey, Christophe ^a   Marsden, Olivier ^a   Bailly, Christophe ^a  

^a ECOLE CENTRALE DE LYON   (France)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC FIELDS; ATMOSPHERIC THERMODYNAMICS; LAMINAR BOUNDARY LAYER; LARGE EDDY SIMULATION; REYNOLDS NUMBER;

COHERENT VORTICES; COMPARISONS WITH MEASUREMENTS; EXIT VELOCITY PROFILE; GRID RESOLUTION; HIGH REYNOLDS NUMBER; LOW DISSIPATIONS; MOMENTUM THICKNESS; TURBULENCE INTENSITY;

FIGHTER AIRCRAFT;

EID: 79953269554     PISSN: 10706631     EISSN: None     Source Type: Journal    
DOI: 10.1063/1.3555634     Document Type: Article

References (61)

1. Batt RG. Some measurements on the effect of tripping the two-dimensional shear layer. AIAA J. 1975, 13:245. AIAJAH, 0001-1452, 10.2514/3.49681, .
2. Hill WG, Jenkins RC, Gilbert BL. Effects of the initial boundary-layer state on turbulent jet mixing. AIAA J. 1976, 14:1513. AIAJAH, 0001-1452, 10.2514/3.61491,
3. Gutmark E, Ho C-M. Preferred modes and the spreading rates of jets. Phys. Fluids 1983, 26:2932. PHFLE6, 1070-6631, 10.1063/1.864058,
4. Raman G, Zaman KB M Q, Rice EJ. Initial turbulence effect on jet evolution with and without tonal excitation. Phys. Fluids A 1989, 1:1240. PFADEB, 0899-8213, 10.1063/1.857347,
5. Crighton DG. Acoustics as a branch of fluid mechanics. J. Fluid Mech. 1981, 106:261. JFLSA7, 0022-1120, 10.1017/S0022112081001602, .
6. Hussain AK M F. Coherent structures-Reality and myth. Phys. Fluids 1983, 26:2816. PHFLE6, 1070-6631, 10.1063/1.864048, .
7. Zaman KB M Q. Far-field noise of a subsonic jet under controlled excitation. J. Fluid Mech. 1985, 152:83. JFLSA7, 0022-1120, 10.1017/S0022112085000581, .
8. Hussain AK M F, Zedan MF. Effects of the initial condition on the axisymmetric free shear layer: Effects of the initial momentum thickness. Phys. Fluids 1978, 21:1100. PHFLE6, 1070-6631, 10.1063/1.862349,
9. Hussain AK M F, Zedan MF. Effects of the initial condition on the axisymmetric free shear layer: Effects of the initial fluctuation level. Phys. Fluids 1978, 21:1475. PHFLE6, 1070-6631, 10.1063/1.862410,
10. Zaman KB M Q. Effect of the initial condition on subsonic jet noise. AIAA J. 1985, 23:1370. AIAJAH, 0001-1452, 10.2514/3.9094, .
11. Bridges JE, Hussain AK M F. Roles of initial conditions and vortex pairing in jet noise. J. Sound Vib. 1987, 117:289. JSVIAG, 0022-460X, 10.1016/0022-460X(87)90540-2,
12. Grosche F-R. Distributions of sound source intensities in subsonic and supersonic jets. Proc. AGARD Conference on Noise Mechanisms , Brussels, 1973, AGARD CP-131-4.
13. Husain ZD, Hussain AK M F. Axisymmetric mixing layer: Influence of the initial and boundary conditions. AIAA J. 1979, 17:48. AIAJAH, 0001-1452, 10.2514/3.61061,
14. Hussain AK M F, Husain ZD. Turbulence structure in the axisymmetric free mixing layer. AIAA J. 1980, 18:1462. AIAJAH, 0001-1452, 10.2514/3.7737,
15. Lepicovsky J, Brown WH. Effects of nozzle exit boundary-layer conditions on excitability of heated free jets. AIAA J. 1989, 27:712. AIAJAH, 0001-1452, 10.2514/3.10170,
16. Raman G, Rice EJ, Reshotko E. Mode spectra of natural disturbances in a circular jet and the effect of acoustic forcing. Exp. Fluids 1994, 17:415. EXFLDU, 0723-4864, 10.1007/BF01877044,
17. Arakeri VH, Krothapalli A, Siddavaram V, Alkislar MB, Lourenco L. On the use of microjets to suppress turbulence in a Mach 0.9 axisymmetric jet. J. Fluid Mech. 2003, 490:75. JFLSA7, 0022-1120, 10.1017/S0022112003005202,
18. Morris PJ, Zaman KB M Q. Velocity measurements in jets with application to noise source modelling. J. Sound Vib. 2010, 329:394. JSVIAG, 0022-460X, 10.1016/j.jsv.2009.09.024,
19. Wygnanski I, Oster D, Fiedler H, Dziomba B. On the perseverance of a quasi-two-dimensional eddy-structure in a turbulent mixing layer. J. Fluid Mech. 1979, 93:325. JFLSA7, 0022-1120, 10.1017/S0022112079001920,
20. Bell JH, Mehta RD. Development of a two-stream mixing layer from tripped and untripped boundary layers. AIAA J. 1990, 28:2034. AIAJAH, 0001-1452, 10.2514/3.10519,
21. Strykowski PJ, Russ S. The effect of boundary-layer turbulence on mixing in heated jets. Phys. Fluids A 1992, 4:865. PFADEB, 0899-8213, 10.1063/1.858265,
22. Russ S, Strykowski PJ. Turbulent structure and entrainment in heated jets: The effect of initial conditions. Phys. Fluids A 1993, 5:3216. PFADEB, 0899-8213, 10.1063/1.858678,
23. Maestrello L, McDaid E. Acoustic characteristics of a high-subsonic jet. AIAA J. 1971, 9:1058. AIAJAH, 0001-1452, 10.2514/3.49917,
24. Antonia RA, Zhao Q. Effect of initial conditions on a circular jet. Exp. Fluids 2001, 31:319. EXFLDU, 0723-4864, 10.1007/s003480100289,
25. Xu G, Antonia RA. Effects of different initial conditions on a turbulent free jet. Exp. Fluids 2002, 33:677. EXFLDU, 0723-4864,
26. Colonius T, Lele SK. Computational aeroacoustics: Progress on nonlinear problems of sound generation. Prog. Aerosp. Sci. 2004, 40:345. PAESD6, 0376-0421, 10.1016/j.paerosci.2004.09.001,
27. Bailly C, Bogey C. Contributions of CAA to jet noise research and prediction. Int. J. Comput. Fluid Dyn. 2004, 18:481. IJCFEC, 1061-8562, 10.1080/10618560410001673498,
28. Wang M, Freund JB, Lele SK. Computational prediction of flow-generated sound. Annu. Rev. Fluid Mech. 2006, 38:483. ARVFA3, 0066-4189, 10.1146/annurev.fluid.38.050304.092036,
29. Freund JB. Noise sources in a low-Reynolds-number turbulent jet at Mach 0.9. J. Fluid Mech. 2001, 438:277. JFLSA7, 0022-1120, 10.1017/S0022112001004414, .
30. Stanley SA, Sarkar S. Influence of nozzle conditions and discrete forcing on turbulent planar jets. AIAA J. 2000, 38:1615. AIAJAH, 0001-1452, 10.2514/2.1144,
31. Bogey C, Bailly C. Effects of inflow conditions and forcing on a Mach 0.9 jet and its radiated noise. AIAA J. 2005, 43:1000. AIAJAH, 0001-1452, 10.2514/1.7465,
32. Keiderling F, Kleiser L, Bogey C. Numerical study of eigenmode forcing effects on jet flow development and noise generation mechanisms. Phys. Fluids 2009, 21:045106. PHFLE6, 1070-6631, 10.1063/1.3112686,
33. Kim J, Choi H. Large eddy simulation of a circular jet: Effect of inflow conditions on the near field. J. Fluid Mech. 2009, 620:383. JFLSA7, 0022-1120, 10.1017/S0022112008004722,
34. Bogey C, Bailly C. Influence of nozzle-exit boundary-layer conditions on the flow and acoustic fields of initially laminar jets. J. Fluid Mech. 2010, 663:507. JFLSA7, 0022-1120, 10.1017/S0022112010003605,
35. Bogey C, Barré S, Bailly C. Direct computation of the noise generated by subsonic jets originating from a straight pipe nozzle. Int. J. Aeroacoust. 2008, 7:1. ZZZZZZ, 1475-472X, 10.1260/147547208784079917,
36. Uzun A, Hussaini M. Investigation of high frequency noise generation in the near-nozzle region of a jet using large eddy simulation. Theor. Comput. Fluid Dyn. 2007, 21:291. TCFDEP, 0935-4964, 10.1007/s00162-007-0048-z,
37. Mohseni K, Colonius T. Numerical treatment of polar coordinate singularities. J. Comput. Phys. 2000, 157:787. JCTPAH, 0021-9991, 10.1006/jcph.1999.6382,
38. Bogey C, Bailly C. A family of low dispersive and low dissipative explicit schemes for flow and noise computations. J. Comput. Phys. 2004, 194:194. JCTPAH, 0021-9991, 10.1016/j.jcp.2003.09.003,
39. Bogey C, de Cacqueray N, Bailly C. Finite differences for coarse azimuthal discretization and for reduction of effective resolution near origin of cylindrical flow equations. J. Comput. Phys. 2011, 230:1134. JCTPAH, 0021-9991, 10.1016/j.jcp.2010.10.031,
40. Bogey C, de Cacqueray N, Bailly C. A shock-capturing methodology based on adaptative spatial filtering for high-order non-linear computations. J. Comput. Phys. 2009, 228:1447. JCTPAH, 0021-9991, 10.1016/j.jcp.2008.10.042,
41. Berland J, Bogey C, Marsden O, Bailly C. High-order, low dispersive and low dissipative explicit schemes for multiple-scale and boundary problems. J. Comput. Phys. 2007, 224:637. JCTPAH, 0021-9991, 10.1016/j.jcp.2006.10.017,
42. Bogey C, Bailly C. Large eddy simulations of transitional round jets: Influence of the Reynolds number on flow development and energy dissipation. Phys. Fluids 2006, 18:065101. PHFLE6, 1070-6631, 10.1063/1.2204060,
43. Bogey C, Bailly C. Large eddy simulations of round free jets using explicit filtering with/without dynamic Smagorinsky model. Int. J. Heat Fluid Flow 2006, 27:603. IJHFD2, 0142-727X, 10.1016/j.ijheatfluidflow.2006.02.008,
44. Bogey C, Bailly C. Turbulence and energy budget in a self-preserving round jet: Direct evaluation using large-eddy simulation. J. Fluid Mech. 2009, 627:129. JFLSA7, 0022-1120, 10.1017/S0022112009005801,
45. Tam CK W, Dong Z. Radiation and outflow boundary conditions for direct computation of acoustic and flow disturbances in a nonuniform mean flow. J. Comput. Acoust. 1996, 4:175. JCOAEJ, 0218-396X, 10.1142/S0218396X96000040,
46. Bogey C, Bailly C. Three-dimensional non reflective boundary conditions for acoustic simulations: Far-field formulation and validation test cases. Acta Acust. 2002, 88:463. ZZZZZZ, 1022-4793,
47. Bogey C, Barré S, Juvé D, Bailly C. Simulation of a hot coaxial jet: Direct noise prediction and flow-acoustics correlations. Phys. Fluids 2009, 21:035105. PHFLE6, 1070-6631, 10.1063/1.3081561,
48. Ahuja KK, Tester BJ, Tanna HK. Calculation of far field jet noise spectra from near field measurements with true source location. J. Sound Vib. 1987, 116:415. JSVIAG, 0022-460X, 10.1016/S0022-460X(87)81374-3,
49. Fleury V, Bailly C, Jondeau E, Michard M, Juvé D. Space-time correlations in two subsonic jets using dual-PIV measurements. AIAA J. 2008, 46:2498. AIAJAH, 0001-1452, 10.2514/1.35561,
50. Lau JC, Morris PJ, Fisher MJ. Measurements in subsonic and supersonic free jets using a laser velocimeter. J. Fluid Mech. 1979, 93:1. JFLSA7, 0022-1120, 10.1017/S0022112079001750,
51. Tanna HK. An experimental study of jet noise. Part I: Turbulent mixing noise. J. Sound Vib. 1977, 50:405. JSVIAG, 0022-460X, 10.1016/0022-460X(77)90493-X, .
52. Bogey C, Barré S, Fleury V, Bailly C, Juvé D. Experimental study of the spectral properties of near-field and far-field jet noise. Int. J. Aeroacoust. 2007, 6:73. ZZZZZZ, 1475-472X, 10.1260/147547207781041868,
53. Davies PO A L, Fisher MJ, Barratt MJ. The characteristics of the turbulence in the mixing region of a round jet. J. Fluid Mech. 1963, 15:337. JFLSA7, 0022-1120, 10.1017/S0022112063000306,
54. Mollo-Christensen E, Kolpin MA, Martucelli JR. Experiments on jet flows and jet noise far-field spectra and directivity patterns. J. Fluid Mech. 1964, 18:285. JFLSA7, 0022-1120, 10.1017/S0022112064000209,
55. Lush PA. Measurements of subsonic jet noise and comparison with theory. J. Fluid Mech. 1971, 46:477. JFLSA7, 0022-1120, 10.1017/S002211207100065X, .
56. Schaffar M. Direct measurements of the correlation between axial in-jet velocity fluctuations and far field noise near the axis of a cold jet. J. Sound Vib. 1979, 64:73. JSVIAG, 0022-460X, 10.1016/0022-460X(79)90573-X, .
57. Panda J, Seasholtz RG, Elam KA. Investigation of noise sources in high-speed jets via correlation measurements. J. Fluid Mech. 2005, 537:349. JFLSA7, 0022-1120, 10.1017/S0022112005005148,
58. Bogey C, Bailly C. An analysis of the correlations between the turbulent flow and the sound pressure field of subsonic jets. J. Fluid Mech. 2007, 583:71. JFLSA7, 0022-1120, 10.1017/S002211200700612X,
59. Tam CK W, Viswanathan K, Ahuja KK, Panda J. The sources of jet noise: Experimental evidence. J. Fluid Mech. 2008, 615:253. JFLSA7, 0022-1120, 10.1017/S0022112008003704,
60. Pope SB. Turbulent Flows 2000, (Cambridge University Press, Cambridge, UK, ).
61. Bailly C, Comte-Bellot G. Turbulence 2003, and, (CNRS, Paris, ).