Shock Oscillations in a Supersonic Jet Exhibiting Antisymmetrical Screech

It was shown that the shocks oscillate at the screech frequency, in a symmetrical or antisymmetrical manner, according to the screech mode. The temporal signals of two diametrically opposed near-field microphones were also considered. At a nozzle pressure ratio of 2.54, corresponding to a flapping m...

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Veröffentlicht in:AIAA journal 2012-09, Vol.50 (9), p.2017-2020
Hauptverfasser: André, Benoît, Castelain, Thomas, Bailly, Christophe
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Sprache:eng
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