Journal of Aeronautical Engineering

Journal of Aeronautical Engineering

Far-field noise prediction for different geometries with Hybrid method

Document Type : Original Article

Authors
1 PhD student, Mechanics, Yazd University, Yazd
2 Professor, Faculty of Mechanical Engineering, Yazd University, Yazd, Iran
Abstract
In this study, to investigating the efficiency of the Curle and the compact form of the acoustic analogy in the far-field noise prediction, the flow around a square, a circular and an elliptic cross-sectional geometry at Reynolds numbers of 46000 and 69000 are simulated in the open-source software, OpenFOAM. The large eddy simulation approach has been used to simulate the incompressible flow around the geometries. To predict the far-field sound pressure levels with the Curle acoustic analogy, the data of the surface pressure fluctuations has been used, which were saved during the simulations through the probe utility of OpenFOAM, while with the compact form of the Curle acoustic analogy, the fluctuations of the lift coefficient have been used. To validate the numerical approach in the study, in the first part of the results, the average aerodynamic coefficients (lift, drag coefficients), mean pressure coefficient, Strouhal number and the formation of the coherent structures of the flow through Q-criterion are investigated.In the second part of the results of the present study, the far-field sound pressure level due to the interaction of the flow with the geometries were investigated. To validate the results in this section, the far-field sound pressure level of the geometry with square cross-section has been investigated and the proper precision of the approach has been evaluated. Finally, the results of the study have shown that the geometry with the square cross-section produces the maximum and the geometry with the elliptical cross-section produces the minimum far-field sound pressure level.
Keywords

[1].S. Becker, M. Escobar, C. Hahn, I. Ali, M. Kaltenbacher, B. Basel, M. Grunewald, “Experimental and Numerical Investigation of the Flow Induced Noise from a Forward Facing Step”,  2005
[2].J.F. Dorneanu, A. Mueller, P. Rambaud, E.T.A.v.d. Weide, A. Hirschberg, “Tonal and Silent Wake Modes of a Square Rod at Incidence”, Acta Acustica united with Acustica, 102(3)419-422, 2016
[3].M. Rawat, R. Gupta, R. Sarviya, “Numerical Simulation of Flow Around An Elliptical Cylinder at High Reynolds Numbers”, International Journal of Fluids Engineering, 5(1) 29-37, 2013
[4].Z. Faruquee, D.S. Ting, A. Fartaj, R.M. Barron, R. Carriveau, “The effects of axis ratio on laminar fluid flow around an elliptical cylinder”, International Journal of Heat and Fluid Flow, 28(5),1178-1189,2007
[5].A. Sharma, P. Kumar, S.K. Singh, “Numerical analysis of flow structures behind the bluff body at different aspect ratio”, in:  IOP Conference Series: Materials Science and Engineering, IOP Publishing,  pp. 012056, 2018
[6].S.K. Raman, K. Arul Prakash, S. Vengadesan, “Effect of axis ratio on fluid flow around an elliptic cylinder—a numerical study”, Journal of fluids engineering, 135(11) ,2013
[7].C.J. Doolan, “Computational bluff body aerodynamic noise prediction using a statistical approach”, Applied Acoustics, 71(12) 1194-1203,2010
[8].E. Latorre Iglesias, D.J. Thompson, M.G. Smith, “Experimental study of the aerodynamic noise radiated by cylinders with different cross-sections and yaw angles”, Journal of Sound and Vibration,361,108-129,2016
[9].J.C. Cai, J. Pan, A. Kryzhanovskyi, S.J. E, “A numerical study of transient flow around a cylinder and aerodynamic sound radiation”, Thermophysics and Aeromechanics, 25(3) 331-346,2018
[10].F. Margnat, “Hybrid prediction of the aerodynamic noise radiated by a rectangular cylinder at incidence”, Computers & Fluids, 109  13-26, 2015
[11].W.S. H. Fujita, H. Furutani, H. Suzuki, “Experimental investigations and prediction of arerodynamic sound generated from square cylinders”, 4th AIAA/CEAS Aeroacoustics Conference, Toulouse, France, pp. 2369-2375,1998
[12].T.F.B. F. V. Hutcheson, “Noise radiation from single and multiple rod configurations”, International Journal of Aeroacoustics, 11, No. 3, pp. 291-333 ,2012
[13].A. Mueller, “Large eddy simulation of cross-flow around a square rod at incidence with application to tonal noise prediction”, 2012.
[14].C.J. Doolan, “Flow and Noise Simulation of the NASA Tandem Cylinder Experiment using OpenFOAM”, In15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference) (p.3157)2009
[15].S.R.L. Samion, M.S.M. Ali, A. Abu, C.J. Doolan, R.Z.-Y. Porteous, “Aerodynamic sound from a square cylinder with a downstream wedge”, Aerospace Science and Technology, 53 ,85-94,2016
[16].ذبیحی نژاد، میلاد. دهقان، علی اکبر. فرمانی، محمد." پیاده سازی و ارزیابی قیاس صوتی کرل به منظور پیش بینی نوفه دوردست برای یک هندسه مربعی"، مجله انجمن مهندسی صوتیات ایران، شماره 1، دوره 9، صفحات 55-69، 1400
[17].C.H.L. X. Jiang, “Numerical techniques for direct and large eddy simulations”, Florida: CRC Press, 4th Edittion, pp. 19-24,2016
[18].M. Lesieur, “Turbulence in Fluids”, 4th Edition, Germany: Springer Science & Buisiness Media,  pp. 419-452,2008
[19].J.C. Y. P. Wang, H. C. Lee, “Accurate simulations of surface pressure fluctuations and flow-induced noise near bluff body at low mach numbers The Seventh International Colloquium on Bluff Body Aerodynamics and Applications” (BBAA7),Shanghai, China,2012
[20].M.J. Lighthill, “On sound generated aerodynamically” I. General theory, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 211(1107) 564-587,1952
[21].C. N, “The influence of solid boundaries upon aerodynamic sound”, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 231(1187) 505-514,1955
[22].C.J. Greenshields, “OpenFOAM user guide”, OpenFOAM Foundation Ltd, version, 3(1) e2888,2015
[23].C. Wagner, T. Hüttl, P. Sagaut, “Large-eddy simulation for acoustics”, Cambridge University Press, 2007
Volume 24, Issue 2
April 2022
Pages 11-26

  • Receive Date 08 January 2022
  • Revise Date 07 February 2022
  • Accept Date 11 February 2022