Browse > Article
http://dx.doi.org/10.1016/j.ijnaoe.2017.02.002

Development of formulation Q1As method for quadrupole noise prediction around a submerged cylinder  

Choi, Yo-Seb (Department of Naval Architecture and Ocean Engineering, Seoul National University)
Choi, Woen-Sug (Department of Naval Architecture and Ocean Engineering, Seoul National University)
Hong, Suk-Yoon (Department of Naval Architecture and Ocean Engineering, Seoul National University)
Song, Jee-Hun (Department of Naval Architecture and Ocean Engineering, Chonnam National University)
Kwon, Hyun-Wung (Department of Naval Architecture and Ocean Engineering, Koje College)
Seol, Han-Shin (Advanced Ship Research Division, Korea Research Institute of Ships and Ocean Engineering)
Jung, Chul-Min (The 6th R&D Institute-3rd Directorate, Agency for Defense Development)
Publication Information
International Journal of Naval Architecture and Ocean Engineering / v.9, no.5, 2017 , pp. 484-491 More about this Journal
Abstract
Recent research has shown that quadrupole noise has a significant influence on the overall characteristics of flow-induced noise and on the performance of underwater appendages such as sonar domes. However, advanced research generally uses the Ffowcs Williams-Hawkings analogy without considering the quadrupole source to reduce computational cost. In this study, flow-induced noise is predicted by using an LES turbulence model and a developed formulation, called the formulation Q1As method to properly take into account the quadrupole source. The noise around a circular cylinder in an underwater environment is examined for two cases with different velocities. The results from the method are compared to those obtained from the experiments and the permeable FW-H method. The results are in good agreement with the experimental data, with a difference of less than 1 dB, which indicates that the formulation Q1As method is suitable for use in predicting quadrupole noise around underwater appendages.
Keywords
Quadrupole noise; Circular cylinder; Acoustic analogy; Formulation Q1As method; OpenFOAM;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
1 Hanson, D.B., Fink, M.R., 1979. The importance of quadrupole sources in prediction of transonic tip speed propeller noise. J. Sound Vib. 62, 19-38.   DOI
2 Ianniello, S., Muscari, R., Di mascio, A., 2014. Ship underwater noise assessment by the acoustic analogy, part II: hydroacoustic analysis of a ship scaled model. J. Mar. Sci. Technol. 19, 52-74.   DOI
3 Jasak, H., 2009. OpenFOAM: open source CFD in research and industry. Int. J. Nav. Archit. Ocean Eng. 1, 89-94.
4 Lighthill, M.J., 1952. On sound generated aerodynamically, I: general theory. Proc. R. Soc. A221, 564-587.
5 Norberg, C., 2003. Fluctuating lift on a circular cylinder: review and new measurement. J. Fluids Struct. 17 (1), 57-96.   DOI
6 OpenFOAM, 2011. OpenFOAM the Open Source CFD Toolbox User Guide, pp. 123-128.
7 Orselli, R.M., Meneghini, J.R., Saltra, F., 2009. Two and Three-dimensional Simulation of Sound Generated by Flow Around a Circular Cylinder. American Institute of Aeronautics and Astronautics, AIAA, pp. 2009-3270.
8 Park, I.C., 2012. 2-dimensional Simulation of Flow-induced Noise Around Circular Cylinder. Thesis and Dissertations. Chungnam University.
9 Schmitz, F.H., Yu, Y.H., 1977. Theoretical modeling of high-speed helicopter impulsive noise. In: Paper Presented at the Third European Rotorcraft and Powered Lift Aircraft Forum, Aix-en-Provence, France.
10 Wang, M., Freund, J.B., Lele, S.K., 2006. Computational prediction of flowgenerated sound. In: Annual Review of Fluid Mechanics, 38, pp. 483-512.   DOI
11 Weller, H.G., Tabor, G., Jasak, H., Fureby, C., 1998. A tensorial approach to computational continuum mechanics using object-oriented techniques. Comput. Phys. 12 (6), 620-631.   DOI
12 Curle, N., 1955. The influence of solid boundaries upon aerodynamic sound. Proc. R. Soc. Lond. Ser. A Math. Phys. Sci. 231 (1187), 505-514.   DOI
13 Zhang, H., Yang, J., Xiao, L., Lu, H., 2015. Large-eddy simulation of the flow past both finite and infinite circular cylinders at Re = 3900. J. Hydrodyn. Ser. B 27, 195-203.   DOI
14 Brentner, K.S., 1997. An efficient and robust method for predicting helicopter rotor high-speed impulsive noise. J. Sound Vib. 203 (1), 87-100.   DOI
15 Ansys, 2009. Ansys Fluent 12.0 Theory Guide, Aerodynamically Generated Noise, pp. 421-432.
16 Brentner, K.S., Farassat, F., 2003. Modeling aerodynamically generated sound of helicopter rotors. Prog. Aerosp. Sci. 39, 83-120.   DOI
17 Choi, W., Choi, Y., Hong, S., Song, J., Kwon, H., Jung, C., 2016. Turbulentinduced noise of a submerged cylinder using a permeable FW-H. Int. J. Nav. Archit. Ocean Eng. 8, 235-242.   DOI
18 Farassat, F., Brentner, K.S., 1987. The uses and abuses of the acoustic analogy in helicopter rotor noise prediction. J. Am. Helicopter Soc. 33, 29-36.
19 Di Francescantonio, D., 1997. A new boundary integral formulation for the prediction of sound radiation. J. Sound Vib. 202 (4), 491-509.   DOI
20 Farassat, F., 2007. Derivation of Formulations 1 and 1A of Farassat. NASA/TM-2007-214853. NASA.
21 Ffowcs Williams, J.E., Hawkings, D.L., 1969. Sound generation by turbulence and surfaces in arbitrary motion. Philos. Trans. R. Soc. Lond. A 264 (1151), 321-342.   DOI