Aeroacoustics Bibliography

[38]
Aybay, O., Caraeni, M. and Holst, S. 2011.”Tandem Cylinder and Idealized Side Mirror Far-Field Noise Predictions Using DES and An Efficient Implementation of FW-H Equation”, 17th AIAA/CEAS Aeroacoustics Conference, AIAA, Portland, Oregon (USA).

[39]
Bailly, C. and Juve, D. 1999. “A Stochastic Approach to Compute Subsonic Noise using Linearized Euler’s Equations”, AIAA Journal, AIAA-99-1872.

[40]
Baris, O., and Mendonca, F. 2011. “Automotive Turbocharger Compressor CFD and Extension Towards Incorporating Installation Effects”, Proceedings of ASME Turbo Expo 2011: Power for Land, Sea, and Air. GT2011-46796.

[41]
Bechara, W., Bailly, C., Lafon, P., and Candel, S. 1994. ”Stochastic approach to Noise Modeling for Free Turbulent Flows“, AIAA Journal, 32:3, pp. 455-463.

[42]
Bechara, W., Lafon, P., Bailly, C., and Candel, S. 1994. ”Application of a k-epsilon turbulence model to the prediction for simple and coaxial free jets“, Journal Acoustics Soc. Am, 97:6, pp. 3518-3531.

[43]
Bodony, D. J. 2006. “Analysis of Sponge Zones for Computational Fluid Mechanics”, Journal of Comp. Physics, 212-2, pp. 681-702.

[44]
Bres, G.A., Brentner, K.S., Perez, G. and Jones, H.E. 2004. “Maneuvering rotorcraft noise prediction”, J Sound and Vibration, 275:3-5, pp. 719-738.

[45]
Brentner, K.S. 1994. “A new algorithm for computing acoustic integrals”, Proceedings of the 14th IMACS World Congress.

[46]
Brentner, K.S. and Farassat, F. 1998. “Analytical comparison of the acoustic analogy and Kirchhoff formulation for moving surfaces”, AIAA Journal, 36:8, pp. 1379-1386.

[47]
Brentner, K.S. and Farassat, F. 2003. “Modeling aerodynamically generated sound of helicopter rotors”, Progress in Aerospace Sciences, 39:2-3, pp. 83-120.

[48]
Caridi, D. 2008. “Industrial CFD Simulation of Aerodynamic Noise”, Doctoral Thesis, University of Naples Federico II.

[49]
Casalino, D. 2003. “An advanced time approach for acoustic analogy predictions”, J Sound and Vibration, 261:4, pp. 583-612.

[50]
Colonius, T. 2004. “Modeling Artificial Boundary Conditions for Compressible Flow”, Annual Review of Fluid Mechanics, 36, pp. 315-345.

[51]
Curle, N. 1955. “The Influence of Solid Boundaries upon Aerodynamic Sound”, Proceedings of the Royal Society of London, series A, Mathematical and Physical Sciences, 231, pp. 505-514.

[52]
De Roeck, W., Baelmans, M., and Desmet, W. 2007. "An Aerodynamic/Acoustic Splitting Technique for Hybrid CAA Applications", AIAA Journal, AIAA-2007-3726.

[53]
De Roeck, W. and Desmet, W. 2007. "Accurate CAA-Simulations using a Low-Mach Aerodynamic/Acoustic Splitting Technique", AIAA Journal, AIAA-2009-3230.

[54]
di Francescantonio, P. 1997. “A new boundary integral formulation for the prediction of sound radiation” J. Sound and Vibration, 202, 491-509.

[55]
Farassat, F. 2007. “Derivation of formulations 1 and 1A of Farassat”, Technical Memorandum TM-2007-214853, NASA, NASA Langley Research Center (USA).

[56]
Farassat F., Padula S.L. and Dunn M.H. 1987. “Advanced Turboprop Noise Prediction Based on Recent Theoretical Results” J. Sound and Vibration, 119:1 pp. 53-79.

[57]
Farassat F., Succi G. P. 1983. “The prediction of helicopter discrete frequency noise” Vertica, 7:4 pp. 309-320.

[58]
Ffowcs Williams, J. and Hawkings, D. 1969. “Sound Generation by Turbulence and Surfaces in Arbitrary Motion”, Philosophical Transactions of Royal Society of London, Series A, Mathematical and Physical Sciences (1934-1990), 264:1151, pp. 321-342.

[59]
Frota, J., Lempereur, P. and Roger, M. 1998. “Computation of the noise of a subsonic propeller at an angle of attack”, 4th AIAA/CEAS Aeroacoustic Conference, AIAA, Toulouse (France).

[60]
Gennaro, M. and Caridi, D. 2010. “Ffowcs Williams-Hawkings Acoustic Analogy for Simulation of NASA SR2 Propeller Noise in Transonic Cruise Condition”, ECCOMAS CFD 2010.

[61]
Greschner, B., Thiele, F., Jacob, M.C., and Casalino, D., 2008. “Prediction of sound generated by a rod-airfoil configuration using EASM DES and the genralise Lighthill/FW-H analogy”, Computers and Fluids, 37, pp. 402-413.

[62]
Goldstein, M.E. 1976. Aeroacoustics, McGraw-Hill, New York.

[63]
Goldstein, M.E. and Rosenbaum, B. 1973. “Effect of Anisotropic Turbulence on Aerodynamic Noise”, J. Acoustical Society of America, 54, pp. 630-645.

[64]
Hinze, J. O. 1975. Turbulence, McGraw-Hill, pp. 672-673.

[65]
Hubbard, H.H. 1995. “Aeroacoustics of Flight Vehicles, Theory and Practice, Volume 1: Noise Sources” NASA Langley Research Center, Hampton, Virginia, pp. 13.

[66]
Karweit, M., Blanc-Benon, P., Juve, D., and Comte-Bellot, G. 1991. ”Simulation of the Propagation of an Acoustic Wave Through a Turbulent Velocity Field: A Study of Phase Variance”, J. Acoustical Society of America, 89:1, pp. 52-62.

[67]
Kim, J. W., Lau, A. S.H., Sandham, N.D. 2010. “Proposed Boundary Conditions for Gust-Airfoil Interaction Noise”, AIAA Journal, 48-11.

[68]
Kraichnan, R.H. 1970. ”Diffusion by a Random Velocity Field”, J. Computational Physics, 13:1, pp. 22-31.

[69]
Lighthill, M. 1952. “On Sound Generated Aerodynamically. I. General Theory”, Proceedings of the Royal Society of London. Series A, Mathematical and Physical Sciences (1934-1190), 211:1107, pp. 564-587.

[70]
Lighthill, M. 1954. “On Sound Generated Aerodynamically. I. Turbulence as a Source of Sound”, Proceedings of the Royal Society of London. Series A, Mathematical and Physical Sciences (1934-1190), 222:1148, pp. 1-32.

[71]
Lilley, G.M. 1993. “The radiated noise from isotropic turbulence revisited”, NASA Contract Report No. 93-75, NASA Langley Research Center.

[72]
Lin, P.H. 2011. “Computational Aero- and Hydro-acoustics by Space-Time Conservation Element and Solution Element Method”, Ph. D. Thesis, Ohio State University.

[73]
Lockard, D. P. 2002. “A Comparison of Ffowcs Williams-Hawkings Solvers for Airframe Noise Applications”, 8th AIAA-/CEAS Aeroacoustics Conference, AIAA-2002-2580.

[74]
Mankbadi, R.R. 1993. “Computational aero- and hydro-acoustics” ASME United Engineering Center.

[75]
Marinus, B. and Roger, M. 2009. “Truncated Method for Propeller Noise Prediction Up to Low Supersonic Helical Tip Mach Numbers”, AIAA-2009-3330.

[76]
Mendonca, F., 2013. "CFD/CAE Combinations in Open Cavity Noise Predictions for Real Vehicle Sunroof Buffeting," SAE Int. J. Passeng. Cars - Mech. Syst. 6(1):360-368

[77]
Mendonca, F., Baris, O., and Capon, G. 2012 “Simulation of Radial Compressor Aeroacoustics Using CFD.”, Effects”, Proceedings of ASME Turbo Expo 2011: Power for Land, Sea, and Air. GT2012-70028.

[78]
Mendonça, F., Read, A., Caro, S., Debatin, K. and Caruelle, B. 2005. “Aeroacoustic Simulation of Double Diaphragm Orifices in an Aircraft Climate Cooling System”, AIAA-2005-2976.

[79]
Pilon A. and Lyrintzis A. 1998. “Development of an Improved Kirchhoff Method for Jet Aeroacoustics”, AIAA Journal, 36:5, pp.783-790.

[80]
Proudman, I. 1952. “The Generation of Noise by Isotropic Turbulence”, Proc. R. Soc. Lond. 214, pp. 119-132.

[81]
Ribner, H.S. 1964. “The Generation of Sound by Turbulent Jets”, in Advances in Applied Mathematics, Academic Press, New York.

[82]
Robinson, A.R. and Lee, D. 1994. “Oceanography and acoustics: prediction and propagation models”, American Institute of Physics.

[83]
Roger, M. 2006 “Fundamentals of aeroacoustics. In Experimental Aeroacoustics”, M. L. Riethmuller and M. R. Lema editors, LS 2007-01. von Karman Institute, Rhode-St-Genese.

[84]
Sarkar, S., Hussaini, M.Y. 1993. “Computation of the Sound Generated by Isotropic Turbulence”, NASA Report 191543, ICASE Report No. 93-74.

[85]
Witkowska, A., and Juve, D. 1993. “Numerical Simulation of Noise Generated by Homogeneous and Isotropic Turbulence,' Proc. 13th Colloquium on Aero- and Hydro-Acoustics, Lyon.

[86]
Wagner, Hüttl, Sagaut (2007). “LES for Acoustics”, Cambridge University Press, ISBN-13: 9780521871440.

[87]
Zhong S., Zhang X, Morfey C., Sandberg R, Fattah R. 2018. "Sound extrapolation methods for turbulent flows based on indirect acoustic variables", AIAA Journal, AIAA-2018-2804.

[88]
Zorumski W.E. and Weir D.S. 1986. “Aircraft Noise Prediction Program Theoretical Manual- Propeller Aerodynamics and Noise” NASA TM-83199, 3.