Aeroacoustic source terms for the linearized euler equations

6th Aeroacoustics Conference and Exhibit

Volumn , Issue , 2000, Pages

  Ewert, Roland ^a   Meinke, Matthias ^a   Schroder, Wolfgang ^a  

^a RWTH AACHEN UNIVERSITY   (Germany)

Author keywords

[No Author keywords available]

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EID: 84894630937     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (24)

1. K. S. Brentner and F. Farassat. An analytical comparison of the acoustic analogy and Kirchhoff formulation for moving surfaces. AIAA Journal, 36:1379-1386, 1998.
2. D.G. Crighton, A.P. Dowling, J.E. Ffowcs Williams, M. Heckl, and F.G. Leppington. Modern Methods in Analytical Acoustics. Springer-Verlag New York Berlin Heidelberg, 1992.
3. J.W. Delfs. Personal cormnunication, 2000.
4. J.W. Delfs, J. Yin, and X. Li. Leading edge noise studies using caa. 1999. AIAA Pap. 99-1897.
5. T.Z. Dong, C.K.W. Tam, and N.N. Reddy. Direct numerical simulation of flap side edge noise. 1999. AIAA Pap. 99-1803.
6. R Ewert, M. Meinke, and W. Schroder. On the computation of the aeroacoustic sound generated by the turbulent flow behind a blunt trailing edge. Comp. Fluid Dynamics Journal, 9/1, To be published April 2000.
7. F. Farassat and M. K. Myers. Extension of Kirchhoff's formula to radiation from moving surfaces. J. of Sound and Vibration, 123(3):451-460, 1988.
8. Y. P. Guo. Application of the Ffowcs Williams/Hawkings equation to two dimensional problems. 403:201-221,2000.
9. J. C. Hardin, J. R. Ristorcelli, and C. K. W. Tam. ICASE/LaRC workshop on benchmark problems in computational aeroacoustics (CAA). Technical Report CP-3300, NASA, Hampton, VA, May 1995.
10. J.C. Hardin and D. S. Pope. An acoustic/viscous splitting technique for computational aeroacoustics. Theoret. Comput. Fluid Dynamics, 6:323-340, 1994.
11. J.C. Hardin and D. S. Pope. Sound generation by flow over a two-dimensional cavity. AIAA Journal, 33/6:407-412, 1995.
12. F. Q. Hu. On perfectly matched layers as an absorbing boundary condition. Technical report, 1996.
13. F. Q. Hu, M. Y. Hussaini, and J. L. Manthey. Low-dissipation and low-dispersion Runge-Kutta schemes for computational acoustics. 124:177-191, 1996.
14. G. M. Lilley. Jet noise classical theory and experiments. In Aeroacoustic of Flight Vehicles: Theory and Practice, 1997. NASA RP-1258.
15. W.H. Lin, A. Hadid, E. Ascoli, and A. Darian. Computation of aeroacoustic solutions by a legendre spectral element method. 1999. AIAA Pap. 99-1944.
16. D.S. Pope. A visous/acoustic splitting technique for aeolian tone prediction. In Second computational aeroacoustic (CAA) workshop on benchmark problems, 1997. NASA CP 3352.
17. H. S. Ribner. New theory of jet-noise generation, directionality and spectra. J. Acoust. Soc. America, 36:245-246, 1959.
18. H. S. Ribner. Perspectives on jet noise. 1981. AIAA Pap. 81-0428.
19. W. Z. Shen and J. N. Sorensen. Aeroacoustic modelling of low-speed flows. Theoret. Comput. Fluid Dynamics, 13:271-289, 1999.
20. W. Z. Shen and J. N. S0rensen. Comment on the aeroacoustic formulation of Hardin and Pope. AIAA Journal, 37:141-143, 1999.
21. C. Tam and Z. Dong. A study of the short wave components in computational acoustics. Technical report, 1993.
22. C. Tam and Z. Dong. Wall boundary condition for high-order finite-difference schemes in computational aeroacoustics-i. Technical report, May 1994.
23. C. Tam and J. Webb. Dispersion-relation- preserving finite difference schemes for computational acoustics. 107:262-281, 1993.
24. K. W. Thompson. Time-dependent boundary conditions for hyperbolic systems, ii. 89:439-461, 1990.