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Large Eddy Simulation of Shock-Cell Noise From a Dual Stream Jet

Pérez Arroyo, Carlos and Puigt, Guillaume and Boussuge, Jean-François and Airiau, Christophe Large Eddy Simulation of Shock-Cell Noise From a Dual Stream Jet. (2016) In: 22nd AIAA/CEAS Aeroacoustics Conference, 30 May 2016 - 1 June 2016 (Lyon, France).

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Official URL: http://dx.doi.org/10.2514/6.2016-2798


This study will present the shock-cell noise results obtained from a large eddy aeroacoustic simulation from a dual stream jet. The primary stream is cold and subsonic with exit Mach number of M p = 0.89 and a Reynolds number of Re p = 0.57 × 10 6 . The secondary stream is cold supersonic and under-expanded with a perfectly expanded Mach number of Ms = 1.20 and Res = 1.66 × 10 6 . The computations are performed with the structured multi-block solver elsA. The aerodynamics and aeroacoustics of the flow are studied and analyzed in detail showing good agreement with experimental fits for the lengthscale and shear layer development, and capturing the broadband shock-cell noise in the near and far fields.

Item Type:Conference or Workshop Item (Paper)
Additional Information:This paper appears in: 22nd AIAA/CEAS Aeroacoustics Conference. eISBN: 978-1-62410-386-5
HAL Id:hal-02299364
Audience (conference):International conference proceedings
Uncontrolled Keywords:
Institution:French research institutions > Centre National de la Recherche Scientifique - CNRS (FRANCE)
Université de Toulouse > Institut National Polytechnique de Toulouse - Toulouse INP (FRANCE)
Université de Toulouse > Université Toulouse III - Paul Sabatier - UT3 (FRANCE)
Other partners > Centre Européen de Recherche et Formation Avancées en Calcul Scientifique - CERFACS (FRANCE)
Laboratory name:
European Commission
Deposited On:27 Sep 2019 14:30

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