Comptes Rendus
Large eddy simulation of serration effects on an ultra-high-bypass-ratio engine exhaust jet
Comptes Rendus. Mécanique, Volume 346 (2018) no. 10, pp. 964-977.

Serrated jet nozzles are considered to be an efficient and practical passive control approach for jet noise. However, some fundamental mechanisms of serration effects on jet noise are not fully understood, especially in terms of the sound source. In this paper, a high-fidelity simulation framework using large-eddy simulation (LES) is demonstrated to predict near-field turbulence and far-field acoustics from an ultra-high-bypass-ratio engine with round and serrated nozzles. Far-field sound is predicted using Ffowcs Willams–Hawkings (FWH) integration. The results show that the serrated nozzle increases mixing near the nozzle and hence the turbulence decay rate, reducing the turbulence level downstream. The serrations shift the energy from the low frequencies to the high frequencies and decrease overall sound pressure levels by about 3 dB over the low-frequency range. Sound sources are analysed based on fourth-order space–time correlations. There are six major source components (R1111, R2222, R3333, R1313, R1212, and R2323) inside the jet shear layers. The serrations are able to reduce the amplitude of these source terms, causing them to decay rapidly to a level below the round nozzle jet within 2D downstream of the nozzle.

Received:
Accepted:
Published online:
DOI: 10.1016/j.crme.2018.07.003
Keywords: Large-eddy simulation, Ultra-high bypass-ratio (UHBPR) engine, Noise reduction, Serrated nozzle

Zhong-Nan Wang 1; James Tyacke 1; Paul Tucker 1

1 Department of Engineering, University of Cambridge, Cambridge CB2 1PZ, UK
@article{CRMECA_2018__346_10_964_0,
     author = {Zhong-Nan Wang and James Tyacke and Paul Tucker},
     title = {Large eddy simulation of serration effects on an ultra-high-bypass-ratio engine exhaust jet},
     journal = {Comptes Rendus. M\'ecanique},
     pages = {964--977},
     publisher = {Elsevier},
     volume = {346},
     number = {10},
     year = {2018},
     doi = {10.1016/j.crme.2018.07.003},
     language = {en},
}
TY  - JOUR
AU  - Zhong-Nan Wang
AU  - James Tyacke
AU  - Paul Tucker
TI  - Large eddy simulation of serration effects on an ultra-high-bypass-ratio engine exhaust jet
JO  - Comptes Rendus. Mécanique
PY  - 2018
SP  - 964
EP  - 977
VL  - 346
IS  - 10
PB  - Elsevier
DO  - 10.1016/j.crme.2018.07.003
LA  - en
ID  - CRMECA_2018__346_10_964_0
ER  - 
%0 Journal Article
%A Zhong-Nan Wang
%A James Tyacke
%A Paul Tucker
%T Large eddy simulation of serration effects on an ultra-high-bypass-ratio engine exhaust jet
%J Comptes Rendus. Mécanique
%D 2018
%P 964-977
%V 346
%N 10
%I Elsevier
%R 10.1016/j.crme.2018.07.003
%G en
%F CRMECA_2018__346_10_964_0
Zhong-Nan Wang; James Tyacke; Paul Tucker. Large eddy simulation of serration effects on an ultra-high-bypass-ratio engine exhaust jet. Comptes Rendus. Mécanique, Volume 346 (2018) no. 10, pp. 964-977. doi : 10.1016/j.crme.2018.07.003. https://comptes-rendus.academie-sciences.fr/mecanique/articles/10.1016/j.crme.2018.07.003/

[1] M.J. Lighthill On sound generated aerodynamically: I. General theory, Proc. R. Soc. Lond. A, Volume 211 (1952), pp. 564-587

[2] S. Martens, Jet noise reduction technology development at GE aircraft engines, in: ICAS 2002 Congress Paper, 842.

[3] P. Jordan; T. Colonius Wave packets and turbulent jet noise, Annu. Rev. Fluid Mech., Volume 45 (2013), pp. 173-195

[4] M.B. Alkistar; A. Krothapalli; G.W. Bulter The effect of streamwise vortices on the aeroacoustics of a Mach 0.9 jet, J. Fluid Mech., Volume 578 (2007), pp. 139-169

[5] K.B.M.Q. Zaman; J.E. Bridges; D.L. Huff Evolution from tabs to chevron technology: a review, Int. J. Aeroacoust., Volume 10 (2011), pp. 685-710

[6] C.E. Tinney; P. Jordan The near pressure field of coaxial subsonic jets, J. Fluid Mech., Volume 611 (2008), pp. 175-204

[7] V.G. Mengle, R. Elkoby, L. Brusniak, Reducing propulsion airframe aeroacoustic interactions with uniquely tailored chevrons: 1. Isolated nozzle, AIAA Paper 2006–2433.

[8] V.G. Mengle, R. Elkoby, L. Brusniak, Reducing propulsion airframe aeroacoustic interactions with uniquely tailored chevrons: 2. Installed nozzle, AIAA Paper 2007–2434.

[9] V.G. Mengle, R. Stoker, L. Brusniak, R. Elkoby, Flapron modification effect on jet-flap interaction noise reduction for chevron nozzles, AIAA Paper 2007–3666.

[10] M.L. Shur; P.R. Spalart; M.K. Strelets; A.K. Travin Towards the prediction of noise from jet engines, Int. J. Heat Fluid Flow, Volume 24 (2003), pp. 551-561

[11] Z.-N. Wang, I.Z. Naqavi, M. Mahak, P. Tucker, X. Yuan, P. Strange, Far field noise prediction for subsonic hot and cold jets using large-eddy simulation, in: ASME Paper GT2014-27290.

[12] Z.-N. Wang, I.Z. Naqavi, M. Mahak, P.G. Tucker, P. Boehning, Large-eddy simulation of the flight stream effects on single stream heated jets, AIAA Paper 2017–0457.

[13] H. Xia; P.G. Tucker Numerical simulation of single-stream jets from a serrated nozzle, Flow Turbul. Combust., Volume 88 (2012), pp. 3-18

[14] J. Tyacke; I. Naqavi; Z.-N. Wang; P.G. Tucker; P. Boehning Predictive LES for jet aeroacoustics: current approach and industrial application, J. Turbomach., Volume 139 (2017) | DOI

[15] J.C. Tyacke, Z.-N. Wang, P.G. Tucker, LES-RANS of installed ultra-high bypass-ratio coaxial jet aeroacoustics with a finite span wing-flap geometry and flight stream – part 1: round nozzle, AIAA Paper 2017–3854.

[16] A. Jameson Formulation of kinetic energy preserving conservative schemes for gas dynamics and direct numerical simulation of one-dimensional viscous compressible flow in a shock tube using entropy and kinetic energy preserving schemes, J. Sci. Comput., Volume 34 (2008), pp. 188-208

[17] Z.-N. Wang; J. Tyacke; P. Tucker Hybrid LES/RANS predictions of flows and acoustics from an ultra-highbypass-ratio serrated nozzle, Note on Numerical Fluid Mechanics and Multidisciplinary Design: Progress in Hybrid RANS-LES Modeling, 2018, pp. 1-12 (in press)

[18] P. Tucker Differential equation-based wall distance computation for DES and RANS, J. Comput. Phys., Volume 190 (2003) no. 1, pp. 229-248 | DOI

[19] P.R. Spalart; S.R. Allmaras A one-equation turbulence model for aerodynamic flows, Rech. Aérosp., Volume 1 (1994), pp. 5-21

[20] Y. Liu; P.G. Tucker; R.M. Kerr Linear and nonlinear model large-eddy simulations of a plane jet, Comput. Fluids, Volume 37 (2008), pp. 439-449

[21] A. Najafi-Yazdi, G.A. Bres, L. Mongeau, An acoustic analogy formulation for moving sources in uniformly moving media, Proc. R. Soc. Lond. A, . | DOI

[22] M.E. Goldstein A generalized acoustic analogy, J. Fluid Mech., Volume 488 (2003), pp. 315-333

[23] S. Karabasov; M. Afsar; T. Hynes; A. Dowling; W. McMullan; C. Pokora; G. Page; J. McGuirk Jet noise: acoustic analogy informed by large eddy simulation, AIAA J., Volume 48 (2010) no. 7, p. 1312

Cited by Sources:

Comments - Policy