A computational study of the effects of nozzle-exit turbulence level on the flow and acoustic fields of a subsonic jet

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https://hal.archives-ouvertes.fr/hal-02352732
Contributor : Christophe Bogey <>
Submitted on : Thursday, November 7, 2019 - 7:52:38 AM
Last modification on : Tuesday, November 19, 2019 - 2:37:32 AM

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Christophe Bogey, Olivier Marsden, Christophe Bailly. A computational study of the effects of nozzle-exit turbulence level on the flow and acoustic fields of a subsonic jet. 17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference), Jun 2011, Portland, United States. ⟨10.2514/6.2011-2837⟩. ⟨hal-02352732⟩

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