LES-based evaluation of a~micro-jet noise reduction concept in static and flight conditions
Matematičeskoe modelirovanie, Tome 23 (2011) no. 11, pp. 48-64.

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The Large-Eddy Simulation (LES) numerical system for jet noise computation established since 2002 is used to explore the relatively new noise-reduction concept (injection of high-pressure micro-jets in the vicinity of the main jet nozzle exit). Simulations performed not only demonstrate a capability of the system to capture the essential features of the flow, turbulence, and the far-field noise alteration caused by the micro-jets, but also to reveal the subtle flow features responsible for the effect of injection on noise. Results obtained are in line with the conclusions of experimental studies regarding efficiency of the micro-jets injection in static conditions and, in particular, suggest that this results in a noise reduction comparable with that from chevrons in the lowfrequency range and in a less pronounced high-frequency penalty. However this advantage of the micro-jets noise-reduction concept is mitigated by results of simulations in flight conditions, for which no experimental data are available. This conclusion makes a practical use of the concept for noise reduction of the aviation engine exhaust jets rather unlikely.
Keywords: computational aeroacoustics, large-eddy simulation.
Mots-clés : jet noise, micro-jets injection
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M. L. Shur; P. R. Spalart; M. Kh. Strelets. LES-based evaluation of a~micro-jet noise reduction concept in static and flight conditions. Matematičeskoe modelirovanie, Tome 23 (2011) no. 11, pp. 48-64. http://geodesic.mathdoc.fr/item/MM_2011_23_11_a4/

[1] Shur M. L., Spalart P. R., Strelets M. Kh., Garbaruk A. V., “Further steps in LES-based noise prediction for complex jets”, AIAA Paper, 2006, 2006-485

[2] Eschricht D., Greschner B., Thiele F., Jacob M. C., “Numerical simulation of jet mixing noise asso ciated with engine exhausts”, Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 104 (2009), 121–146 | DOI

[3] Xia H., Tucker P. G., Eastwood S., “Large-eddy simulations of chevron jet flows with noise predictions”, International Journal of Heat and Fluid Flow, 30:6 (2009), 1067–1079 | DOI

[4] Uzun A., Hussaini M. J., “High-fidelity numerical simulation of a chevron nozzle jet flow”, AIAA Paper, 2009, 2009-3194

[5] Mendez S., Shoeybi M., Sharma A., Ham F. E., Lele S. K., Moin P., “Large-eddy simulations of perfectly-expanded supersonic jets: Quality assessment and validation flow”, AIAA Paper, 2010, 2010-271

[6] Shur M. L., Spalart P. R., Strelets M. Kh., “Noise prediction for increasingly complex jets. I: Methods and tests”, International Journal of Aeroacoustics, 4:3 (2005), 213–246 ; “II: Applications”:4, 247–266 | DOI

[7] Shur M. L., Spalart F. R., Strelets M. Kh., “Raschet shuma slozhnykh strui na osnove ‘`pervykh printsipov’ ”, Matematicheskoe modelirovanie, 19:7 (2007), 5–26 | Zbl

[8] Shur M. L., Spalart P. R., Strelets M. Kh., Garbaruk A. V., “Analysis of jet-noise-reduction concepts by large-eddy simulation”, International Journal of Aeroacoustics, 6:3 (2007), 243–285 | DOI

[9] Spalart P. R., Shur M. L., “Variants of the Ffowcs Williams-Hawkings equation and their coupling with simulations of hot jets”, International Journal of Aeroacoustics, 8:5 (2009), 477–492 | DOI

[10] Viswanathan K., Shur M. L., Spalart P. R., Strelets M. Kh., “Flow and noise predictions for single and dual-stream beveled nozzles”, AIAA Journal, 46:3 (2008), 601–626 | DOI | MR

[11] Viswanathan K., Shur M. L., Spalart P. R., Strelets M. Kh., “Comparisons between experiment and large-eddy simulation for jet noise”, AIAA Journal, 45:8 (2007), 1952–1966 | DOI

[12] Spalart P. R., Shur M. L., Strelets M. Kh., “Added sound sources in jets; theory and simulation”, International Journal of Aeroacoustics, 8:6 (2009), 511–534 | DOI

[13] Uzun A., Hussaini M. J., “Simulation of noise generation in near-nozzle region of a chevron nozzle jet”, AIAA Journal, 47:8 (2009), 1793–1810 | DOI

[14] Uzun A., Hussaini M. J., “High-fidelity numerical simulations of a round nozzle jet flow”, AIAA Paper, 2010, 2010-4016

[15] Krothapalli A., Greska B., Arakeri V., “High speed jet noise reduction using microjets”, AIAA Paper, 2002, 2002-2450

[16] Greska B., Krothapalli A., Burnside N., Horne W., “High-speed jet noise reduction using microjets on a jet engine”, AIAA Paper, 2004, 2004-2969

[17] Arakeri V. H., Krothapalli A., Siddavaram V., Alkislar M. B., Lourenco L. M., “On the use of microjets to suppress turbulence in a Mach 0.9 axisymmetric jet”, Journal of Fluid Mechanics, 490 (2003), 75–98 | DOI | Zbl

[18] Alkislar M. B., Krothapalli A., Butler G. W., “The effect of streamwise vortices on the aeroacoustics of a Mach 0.9 jet”, Journal of Fluid Mechanics, 578 (2007), 139–169 | DOI | Zbl

[19] Castelain T., Sunyach M., Juve D., Bera J.-C., “Jet-noise reduction by impinging microjets: an acoustic investigation testing microjet parameters”, AIAA Journal, 46:5 (2008), 1081–1087 | DOI

[20] Huet M., Vuillot F., Rahier G., “Numerical study of the influence of temperature and micro-jets on subsonic jet noise”, AIAA Paper, 2008, 2008-3029

[21] Huet M., Fayard D., Rahier G., Vuillot F., “Numerical investigation of the micro-jets efficiency for jet noise reduction”, AIAA Paper, 2009, 2009-3127

[22] Lew P.-T., Najafiyazdi A., Mongeau L., “Unsteady numerical simulation of a round jet with impinging microjets for noise suppression”, AIAA Paper, 2010, 2010-18