Contents

  1. libAcoustics library brief
  2. Published papers related to libAcoustics technology
  3. Available versions of the library
  4. For citation

libAcoustics library brief

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libAcoustics - library for far-field noise computation. At current time contains 3 kind of far-field predictions:

  1. Curle analogy

  2. Ffowcs Williams Hawkings analogy

  3. CFD-BEM coupling

Available versions of the library

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The library is available for next OpenFOAM versions:

  • OpenFOAM 3.0, 4.1 versions are stored in the master branch
  • OpenFOAM+ v.1812 is in the digitef-dev-1812 branch of the repository
  • OpenFOAM+ v.1912 is in the digitef-dev-1912 branch of the repository
  • OpenFOAM+ v.2012 is in the digitef-dev-2012 branch of the repository

Published papers related to libAcoustics library

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Title Description
A Computational Study on the Aeroacoustics of a Multi-Rotor Unmanned Aerial System: Article Unmanned Aerial System
Numerical Study of Iced Airfoil Aeroacoustics Using IDDES: Article Q-criterion around wing
Wall-modeled large-eddy simulation of a trailing-edge serration–finlet configuration: Article Streamwise vector plots in the serration–finlet configuration
The Eulerian–Lagrangian Approach for the Numerical Investigation of an Acoustic Field Generated by a High-Speed Gas-Droplet Flow: Article Jet with particles Logo
Jet Noise in Airframe Integration and Shielding: Article Emittance of acoustic waves by jet near wing
Validation of the developed open-source library for far-field noise prediction: Article Domain parameters: (a) boundary conditions; (b) mesh configuration and FW-H surface.
Broadband noise prediction using large eddy simulation and a frequency domain method): Article Span-wise vorticity contour
The numerical simulation of compressible jet at low Reynolds number using OpenFOAM: Article Sound pressure level directivity distributions for M = 0.9, Re = 3600
Wing airfoil selection and optimization for the tourist class reusable space vehicle: Article ---
Coupled CFD-based Shape Optimization of a Wing of Reusable Space Vehicle of Tourist Class: Article Computational scheme
Transient cavitating flow structure and acoustic analysis of a hydrofoil with whalelike wavy leading edge: Article Flow fields around wing
A proposed wavy shield for suppression of supersonic jet noise utilizing reflections Acoustic fields
Numerical Study of Flow-Induced Noise around Cylinder and Rod-NACA0012 Hydrofoil ---
Simulations of Noise Generated by Rotor-Rotor Interactions at Static Conditions ---
Investigating the Impact of Water Injection on Noise Generation During Rocket Lift-Off ---
Prediction of the Free Jet Noise Using Quasi-gas Dynamic Equations and Acoustic Analogy: Article QGDFoam instant jet velocities
Simulations of Broadband Noise of a Small UAV Propeller: Article ---
Analysis Methods and Design Measures for the Reduction of Noise and Vibration Induced by Marine Propellers: Article Vortices after propeller thruster
Prediction of Noise Associated with an Isolated UAV Propeller: MSc Thesis Velocity vectors around wing
High-Fidelity Simulations of Noise Generation in a Propeller-Driven Unmanned Aerial Vehicle: Article ---
Análise e validação de modelo de simulação numérica para previsão de ruído aerodinâmico utilizando OpenFOAM e Libacoustics: MSc Thesis acoustic field around tandem

For citation

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If you have found the software useful for your research, please cite next sources:

  • DOI

  • Epikhin, A., Evdokimov, I., Kraposhin, M., Kalugin, M., Strijhak, S. Development of a Dynamic Library for Computational Aeroacoustics Applications Using the OpenFOAM Open Source Package // Procedia Computer ScienceVolume 66, 2015, Pages 150-157 https://www.sciencedirect.com/science/article/pii/S1877050915033670 , DOI: 10.1016/j.procs.2015.11.018