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Open source codes/programs of acoustic analogies to calculate subsonic and supersonic noise characteristics induced by unsteady flow, moving geometry and mutual interactions either in a stationary or a moving medium. A permeable interface with arbitrary mesh is adopted to enclose the nonlinear region calculated by unsteady CFD solvers (Fluent).

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References of acoustic prediction

  1. Ghorbaniasl G, Lacor C. A moving medium formulation for prediction of propeller noise at incidence[J]. Journal of Sound & Vibration, 2012, 331(1):117-137.
  2. Casalino D. An advanced time approach for acoustic analogy predictions[J]. Journal of Sound & Vibration, 2003, 261(4):583-612.
  3. Development & validation of the acoustic analogy code for jet noise predictions.
  4. Prieur J, Rahier G. Aeroacoustic integral methods, formulation and efficient numerical implementation[J]. Aerospace Science & Technology, 2001, 5(7).
  5. Huang, Zhongjie, Siozos-Rousoulis, etc. Helicopter rotor noise prediction using a convected FW-H equation in the frequency domain[J]. Applied Acoustics, 2018.

References of acoustic scattering

  1. Lee, S. Prediction of acoustic scattering in the time domain and its applications to rotorcraft noise[D]. 2009.

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Open source codes/programs of acoustic analogies to calculate subsonic and supersonic noise characteristics induced by unsteady flow, moving geometry and mutual interactions either in a stationary or a moving medium. A permeable interface with arbitrary mesh is adopted to enclose the nonlinear region calculated by unsteady CFD solvers (Fluent).

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