ACTA AERONAUTICAET ASTRONAUTICA SINICA >
Large eddy simulation of ideally expanded supersonic jet noise
Received date: 2021-08-23
Revised date: 2021-09-06
Accepted date: 2021-11-03
Online published: 2021-11-10
Supported by
National Natural Science Foundation of China(11872094)
To investigate the influence of the subgrid model and thermal effect on the flowfield and sound field of the supersonic jet， parameter studies are performed by using the LES/FW-H hybrid method. First， the reliability of the LES/FW-H hybrid method is verified through comparison of the numerical simulation and the experimental data. Meanwhile， the noise differences between the simulation and experimental results are studied， and the comparison with Tam’s similarity spectra shows that the differences are resulted from the broadband shock-associated noise. Then， the influences of the subgrid model on the mean flowfield， turbulence statistics， and noise characteristics are discussed. The comparisons indicate that the simulation results of the dynamic Smagorinsky model are consistent with those of the implicit subgrid model， both of which are consistent with the existing experiments and numerical simulations. However， the simulation with the constant Smagorinsky model leads to obvious deviations in the flowfield and the sound field. Finally， the influences of the thermal effect on the flowfield and the sound field of the ideally expanded supersonic jet are studied by changing the total temperature at the nozzle exit. It is found that the total temperature increase intensifies the non-dimensional streamwise velocity fluctuation in the high-frequency range and also enhances the far-field high-frequency noise.
Fangcheng SHI , Zhenxun GAO , Yuyan TIAN , Chongwen JIANG , Tiantian WANG , Chun-Hian LEE . Large eddy simulation of ideally expanded supersonic jet noise[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023 , 44(2) : 626266 -626266 . DOI: 10.7527/S1000-6893.2021.26266
| 1 | 冷岩， 钱战森， 杨龙. 均匀各向同性大气湍流对声爆传播特性的影响［J］. 航空学报， 2020， 41（2）： 123290. |
| LENG Y， QIAN Z S， YANG L. Homogeneous isotropic atmospheric turbulence effects on sonic boom propagation［J］. Acta Aeronautica et Astronautica Sinica， 2020， 41（2）： 123290 （in Chinese）. | |
| 2 | 张俊龙， 雷红胜， 田昊， 等. 亚声速矩形射流的噪声辐射特性和声源分布［J］. 航空学报， 2020， 41（2）： 123386. |
| ZHANG J L， LEI H S， TIAN H， et al. Noise radiation characteristics and source distribution of subsonic rectangular jet［J］. Acta Aeronautica et Astronautica Sinica， 2020， 41（2）： 123386 （in Chinese）. | |
| 3 | HUFF D L. NASA glenn’s contributions to aircraft engine noise research［J］. Journal of Aerospace Engineering， 2013， 26（2）： 218-250. |
| 4 | COLONIUS T， LELE S K. Computational aeroacoustics： Progress on nonlinear problems of sound generation［J］. Progress in Aerospace Sciences， 2004， 40（6）： 345-416. |
| 5 | FREUND J B， LELE S K， MOIN P. Numerical simulation of a Mach 1.92 turbulent jet and its sound field［J］. AIAA Journal， 2000， 38（11）： 2023-2031. |
| 6 | SHARAN N， BELLAN J R. Direct numerical simulation of high-pressure free jets［C］∥AIAA Scitech 2021 Forum. Reston： AIAA， 2021. |
| 7 | MILLER S A. Towards a comprehensive model of jet noise using an acoustic analogy and steady RANS solutions［C］∥19th AIAA/CEAS Aeroacoustics Conference. Reston： AIAA， 2013. |
| 8 | BAI B H， LI X D， CHEN H X. A semi-empirical prediction method for the fine scale turbulence mixing noise［C］∥25th AIAA/CEAS Aeroacoustics Conference. Reston： AIAA， 2019. |
| 9 | MANKBADI R R， HAYER M E， POVINELLI L A. Structure of supersonic jet flow and its radiated sound［J］. AIAA Journal， 1994， 32（5）： 897-906. |
| 10 | DEBONIS J R， SCOTT J N. Large-eddy simulation of a turbulent compressible round jet［J］. AIAA Journal， 2002， 40（7）： 1346-1354. |
| 11 | BODONY D， RYU J， RAY P， et al. Investigating broadband shock-associated noise of axisymmetric jets using large-eddy simulation［C］∥12th AIAA/CEAS Aeroacoustics Conference， 27th AIAA Aeroacoustics Conference）. Reston： AIAA， 2006. |
| 12 | MENDEZ S， SHOEYBI M， SHARMA A， et al. Large-eddy simulations of perfectly expanded supersonic jets using an unstructured solver［J］. AIAA Journal， 2012， 50（5）： 1103-1118. |
| 13 | LO S C， AIKENS K M， BLAISDELL G A， et al. Numerical investigation of 3-D supersonic jet flows using large-eddy simulation［J］. International Journal of Aeroacoustics， 2012， 11（7&8）： 783-812. |
| 14 | SHUR M L， SPALART P R， STRELETS M K， et al. Analysis of jet-noise-reduction concepts by large-eddy simulation［J］. International Journal of Aeroacoustics， 2007， 6（3）： 243-285. |
| 15 | VISWANATHAN K， SHUR M， SPALART P R， et al. Flow and noise predictions for single and dual-stream beveled nozzles［J］. AIAA Journal， 2008， 46（3）： 601-626. |
| 16 | LIU J H， KAILASANATH K， RAMAMURTI R， et al. Large-eddy simulations of a supersonic jet and its near-field acoustic properties［J］. AIAA Journal， 2009， 47（8）： 1849-1865. |
| 17 | AIKENS K M， BLAISDELL G A， LYRINTZIS A S. Analysis of converging-diverging beveled nozzle jets using large eddy simulation with a wall model［C］∥53rd AIAA Aerospace Sciences Meeting. Reston： AIAA， 2015. |
| 18 | NONOMURA T， NAKANO H， OZAWA Y， et al. Large eddy simulation of acoustic waves generated from a hot supersonic jet［J］. Shock Waves， 2019， 29（8）： 1133-1154. |
| 19 | CODERONI M， LYRINTZIS A S， BLAISDELL G A. Large-eddy simulations analysis of supersonic heated jets with fluid injection for noise reduction［J］. AIAA Journal， 2019， 57（8）： 3442-3455. |
| 20 | SAGAUT P. Large eddy simulation for incompressible flows［M］. Berlin： Springer Berlin Heidelberg， 2002. |
| 21 | UZUN A， LYRINTZIS A， BLAISDELL G. Coupling of integral acoustics methods with LES for jet noise prediction［C］∥42nd AIAA Aerospace Sciences Meeting and Exhibit. Reston： AIAA， 2004. |
| 22 | LO S C， BLAISDELL G， LYRINTZIS A， et al. Numerical investigation of 3-D supersonic jet flows using large-eddy simulation［J］. International Journal of Aeroacoustics， 2012， 11（7&8）： 783-812. |
| 23 | JUNQUEIRA-JUNIOR C， YAMOUNI S， AZEVEDO J L F， et al. Influence of different subgrid-scale models in low-order LES of supersonic jet flows［J］. Journal of the Brazilian Society of Mechanical Sciences and Engineering， 2018， 40（5）： 258. |
| 24 | ZHAO W， FRANKEL S H， MONGEAU L. Large eddy simulations of sound radiation from subsonic turbulent jets［J］. AIAA Journal， 2001， 39（8）： 1469-1477. |
| 25 | UZUN A， BLAISDELL G A， LYRINTZIS A S. Sensitivity to the smagorinsky constant in turbulent jet simulations［J］. AIAA Journal， 2003， 41（10）： 2077-2079. |
| 26 | ANDERSSON N， ERIKSSON L E， DAVIDSON L. Effects of inflow conditions and subgrid model on LES for turbulent jets［C］∥11th AIAA/CEAS Aeroacoustics Conference. Reston： AIAA， 2005. |
| 27 | BOGEY C， BAILLY C. Decrease of the effective Reynolds number with eddy-viscosity subgrid modeling［J］. AIAA Journal， 2005， 43（2）： 437-439. |
| 28 | SHUR M L， SPALART P R， STRELETS M K. Noise prediction for increasingly complex jets. part I： Methods and tests［J］. International Journal of Aeroacoustics， 2005， 4（3）： 213-245. |
| 29 | BOGEY C， BAILLY C. Large eddy simulations of round free jets using explicit filtering with/without dynamic Smagorinsky model［J］. International Journal of Heat and Fluid Flow， 2006， 27（4）： 603-610. |
| 30 | UZUN A， BLAISDELL G A， LYRINTZIS A S. Impact of subgrid-scale models on jet turbulence and noise［J］. AIAA Journal， 2006， 44（6）： 1365-1368. |
| 31 | TAM C K W， PASTOUCHENKO N N， VISWANATHAN K. Fine-scale turbulence noise from hot jets［J］. AIAA Journal， 2005， 43（8）： 1675-1683 |
| 32 | BRIDGES J. Effect of heat on space-time correlations in jets［C］∥12th AIAA/CEAS Aeroacoustics Conference， 27th AIAA Aeroacoustics Conference. Reston： AIAA， 2006. |
| 33 | LAU J C. Effects of exit Mach number and temperature on mean-flow and turbulence characteristics in round jets［J］. Journal of Fluid Mechanics， 1981， 105： 193-218. |
| 34 | LOPEZ RODRIGUEZ O， SALEEM M， GUTMARK E J， et al. Study of temperature effect on flow and acoustic behavior of supersonic jet emanating from a faceted nozzle［C］∥AIAA Scitech 2021 Forum. Reston： AIAA， 2021. |
| 35 | NAKANO H， NONOMURA T， OYAMA A， et al. Quantitative evaluation of effect of jet temperature on acoustic waves from supersonic jets at Mach 2.0 by large eddy simulations［C］∥2018 AIAA Aerospace Sciences Meeting. Reston： AIAA， 2018. |
| 36 | SEINER J M， PONTON M K， JANSEN B J， et al. The effects of temperature on supersonic jet noise emission［C］∥14th DGLR/AIAA Aeroacoustics Conference， 1992. |
| 37 | VISWANATHAN K. Aeroacoustics of hot jets［C］∥8th AIAA/CEAS Aeroacoustics Conference & Exhibit. Reston： AIAA， 2002. |
| 38 | TANNA H K. An experimental study of jet noise part I： Turbulent mixing noise［J］. Journal of Sound and Vibration， 1977， 50（3）： 405-428. |
| 39 | BHAT T. Reynols number and temperature effects on jet noise［C］∥13th AIAA/CEAS Aeroacoustics Conference， 28th AIAA Aeroacoustics Conference. Reston： AIAA， 2007. |
| 40 | HOCH R G， DUPONCHEL J P， COCKING B J， et al. Studies of the influence of density on jet noise［J］. Journal of Sound and Vibration， 1973， 28（4）： 649-668. |
| 41 | GARNIER E， ADAMS N， SAGAUT P. Boundary conditions for large-eddy simulation of compressible flows［M］∥Scientific computation. Dordrecht： Springer Netherlands， 2009： 155-184. |
| 42 | POPE S B. Turbulent flows［M］. Cambridge： Cambridge University Press， 2000. |
| 43 | ADAMS N A. The role of deconvolution and numerical discretization in subgrid-scale modeling［M］∥Direct and large-eddy simulation IV. Dordrecht： Springer Netherlands， 2001： 311-320. |
| 44 | NONOMURA T， TERAKADO D， ABE Y， et al. A new technique for freestream preservation of finite-difference WENO on curvilinear grid［J］. Computers & Fluids， 2015， 107： 242-255. |
| 45 | MOIN P， SQUIRES K， CABOT W， et al. A dynamic subgrid-scale model for compressible turbulence and scalar transport［J］. Physics of Fluids A： Fluid Dynamics， 1991， 3（11）： 2746-2757. |
| 46 | FFOWCS WILLIAMS J E， HAWKINGS D L. Sound generation by turbulence and surfaces in arbitrary motion［J］. Philosophical Transactions of the Royal Society of London Series A， Mathematical and Physical Sciences， 1969， 264（1151）： 321-342. |
| 47 | SHI F C， GAO Z X， JIANG C W， et al. Numerical investigation of shock-turbulent mixing layer interaction and shock-associated noise［J］. Physics of Fluids， 2021， 33（2）： 025105. |
| 48 | SHI F C， GAO Z X， JIANG C W， et al. Investigation on noise from shock/isotropic turbulence interaction using direct numerical simulation［J］. Journal of Sound and Vibration， 2020， 488： 115633. |
| 49 | SHU C W， OSHER S. Efficient implementation of essentially non-oscillatory shock-capturing schemes［J］. Journal of Computational Physics， 1988， 77（2）： 439-471. |
| 50 | LIOU M S. A sequel to AUSM： AUSM+ ［J］. Journal of Computational Physics， 1996， 129（2）： 364-382. |
| 51 | BRIDGES J， WERNET M. Turbulence associated with broadband shock noise in hot jets［C］∥14th AIAA/CEAS Aeroacoustics Conference， 29th AIAA Aeroacoustics Conference. Reston： AIAA， 2008. |
| 52 | BOGEY C， MARSDEN O. Influence of nozzle-exit boundary-layer profile on high-subsonic jets［C］∥20th AIAA/CEAS Aeroacoustics Conference. Reston： AIAA， 2014. |
| 53 | WHITE F M. Viscous fluid flow［M］. 3rd ed. New York： McGraw-Hill Higher Education， 2006. |
| 54 | BOGEY C， BAILLY C. Influence of nozzle-exit boundary-layer conditions on the flow and acoustic fields of initially laminar jets［J］. Journal of Fluid Mechanics， 2010， 663： 507-538. |
| 55 | LAU J C， MORRIS P J， FISHER M J. Measurements in subsonic and supersonic free jets using a laser velocimeter［J］. Journal of Fluid Mechanics， 1979， 93： 1-27. |
| 56 | HUSSEIN H J， CAPP S P， GEORGE W K. Velocity measurements in a high-Reynolds-number， momentum-conserving， axisymmetric， turbulent jet［J］. Journal of Fluid Mechanics， 1994， 258： 31-75. |
| 57 | SHARMA A， BHASKARAN R， LELE S K. Large-eddy simulation of supersonic， turbulent mixing layers downstream of a splitter plate［C］∥49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston： AIAA， 2011. |
| 58 | TAM C K W， GOLEBIOWSKI M， SEINER J. On the two components of turbulent mixing noise from supersonic jets［C］∥Aeroacoustics Conference. Reston： AIAA， 1996. |
| 59 | TAM C K W， ZAMAN K B M Q. Subsonic jet noise from nonaxisymmetric and tabbed nozzles［J］. AIAA Journal， 2000， 38（4）： 592-599. |
| 60 | VISWANATHAN K. Scaling laws and a method for identifying components of jet noise［J］. AIAA Journal， 2006， 44（10）： 2274-2285. |
| 61 | TAM C K W， HORNE W C， BURNSIDE N J， et al. Spectral analysis of the acoustic near field of a solid-propellant rocket［J］. AIAA Journal， 2017， 56（3）： 949-963. |
| 62 | NORUM T D， SEINER J M. Measurements of mean static pressure and far-field acoustics of shock-containing supersonic jets： NASA-TM-84521 ［R］.Washington， D.C.： NASA， 1982. |
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