Abstract
A two-way coupling on unstructured meshes between a flow and a high-order acoustic solvers for jet noise prediction is considered. The flow simulation aims at generating acoustic sources in the near field while the acoustic simulation solves the full Euler equations, thanks to a discontinuous Galerkin method, in order to take into account nonlinear acoustic propagation effects. This methodology is firstly validated on academic cases involving nonlinear sound propagation, shock waves and convection of aerodynamic perturbations. The results are compared to analytical solutions and direct computations. A good behaviour of the coupling is found regarding the targeted space applications. An application on a launch pad model is then simulated to demonstrate the robustness and reliability of the present approach.
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Acknowledgements
This study is supported by the french national space agency CNES and the ONERA’s scientific direction. The authors are grateful to H. Lambaré, technical referee at CNES for launchers acoustic environment. Special thanks go to J. Troyes from ONERA for his technical support during all this work.
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Financial support for the first author was provided by ONERA and CNES under convention No. 5100015478.
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Langenais, A., Vuillot, F., Peyret, C. et al. Assessment of a Two-Way Coupling Methodology Between a Flow and a High-Order Nonlinear Acoustic Unstructured Solvers. Flow Turbulence Combust 101, 681–703 (2018). https://doi.org/10.1007/s10494-018-9928-0
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DOI: https://doi.org/10.1007/s10494-018-9928-0