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Communication Dans Un Congrès Année : 2009

Influence of the Nozzle-Exit Boundary-Layer Thickness on the Flow and Acoustic Fields of Initially Laminar Jets

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hal-02352706 , version 1 (07-11-2019)

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Christophe Bogey, Christophe Bailly. Influence of the Nozzle-Exit Boundary-Layer Thickness on the Flow and Acoustic Fields of Initially Laminar Jets. 15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference), May 2009, Miami, United States. ⟨10.2514/6.2009-3409⟩. ⟨hal-02352706⟩
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