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Comparison of computational aeroacoustics with theory using the benchmark case of sound waves excited from a semi-infinite duct

  1. Daniel Morgenweck*,
  2. Christoph Schemel,
  3. Frank Thiele

Article first published online: 13 DEC 2004

DOI: 10.1002/pamm.200410245

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PAMM

PAMM

Volume 4, Issue 1, pages 528–529, December 2004

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How to Cite

Morgenweck, D., Schemel, C. and Thiele, F. (2004), Comparison of computational aeroacoustics with theory using the benchmark case of sound waves excited from a semi-infinite duct. Proc. Appl. Math. Mech., 4: 528–529. doi: 10.1002/pamm.200410245

Author Information

  1. Hermann Föttinger Institut für Strömungsmechnik, Müller Breslau Str. 8, 10623 Berlin

*Phone: +49 30 314 24733

Publication History

  1. Issue published online: 13 DEC 2004
  2. Article first published online: 13 DEC 2004

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References

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    Munt, R. M.:, “The interaction of sound with a subsonic jet issuing from a semi-infinite cylindrical pipe” (1977), J. Fluid Mechanics, Vol. 83, part 4, 641-671.
  • [2]
    Tam, C. K. W. and Hardin, J. C.: “Second Computational Aeroacoustic (CAA) Workshop on Benchmark Problems” (1997), Benchmark problem 2, problem 2.
  • [3]
    Tam, C. K. W. and Webb, J. C.: “Dispersion-Relation-Preserving Finite Difference Schemes for Computational Acoustics” (1993), J. Comp. Physics, 107, 262-281.
  • [4]
    Hu, F.Q.; Hussaini, M.Y. and Manthey, J.L.: “Low-Dissipation and Low-Dispersion Runge-Kutta Schemes for Computational Acoustics” (1996), J. Comp. Physics, 124, 177-191.
  • [5]
    Rung, T.; Eschricht, D.; Yan, J. and Thiele, F.: “Sound Radiation of the Vortex Flow past a generic Side Mirror” (2002), AIAA Paper, 2002-2340.
  • [6]
    Stanescu, D. and Habashi, W. G.: “2N-storage Low-dissipation and Low-dispersion Runge-Kutta Schemes for Computational Aeroacoustics” (1998), J. Comput. Phys. Vol. 143, No. 2, 674-681.
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