17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference) 2011
DOI: 10.2514/6.2011-2852
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Validation of Methods to Predict Vibration of a Panel in the Near Field of a Hot Supersonic Rocket Plume

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Cited by 7 publications
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“…[1][2][3][4] Noise from rocket and jet engine exhaust is extensively studied, and the source of sound is predominantly from turbulence and turbulent flow structures interacting with shock waves. [5][6][7][8][9] The particulates within the flow are convecting supersonically, interacting with the turbulence and shock waves, and are an additional source of acoustic radiation. Furthermore, the particulates alter the turbulence and have an effect on the shock cell structure.…”
Section: Introductionmentioning
confidence: 99%
“…[1][2][3][4] Noise from rocket and jet engine exhaust is extensively studied, and the source of sound is predominantly from turbulence and turbulent flow structures interacting with shock waves. [5][6][7][8][9] The particulates within the flow are convecting supersonically, interacting with the turbulence and shock waves, and are an additional source of acoustic radiation. Furthermore, the particulates alter the turbulence and have an effect on the shock cell structure.…”
Section: Introductionmentioning
confidence: 99%