Direct Noise Computation of a Shocked and Heated Jet at a Mach Number of 3.30

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Submitted on : Thursday, November 7, 2019 - 7:49:55 AM
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Nicolas de Cacqueray, Christophe Bogey, Christophe Bailly. Direct Noise Computation of a Shocked and Heated Jet at a Mach Number of 3.30. 16th AIAA/CEAS Aeroacoustics Conference, Jun 2010, Stockholm, Sweden. ⟨10.2514/6.2010-3732⟩. ⟨hal-02352728⟩

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