2018 AIAA/CEAS Aeroacoustics Conference 2018
DOI: 10.2514/6.2018-3790
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An Attempt to Reduce Airfoil Tonal Noise Using Fluid-Structure Interaction

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Cited by 3 publications
(1 citation statement)
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“…For the present study, we used time averaged solution as the base flow for LSA. The time averaged solution was obtained from DAS of the rigid airfoil [26]. Quality of time averaged solution as a base flow was evaluated by LSA without any perturbation and the deviation from its initial state was checked.…”
Section: Linear Stability Analysismentioning
confidence: 99%
“…For the present study, we used time averaged solution as the base flow for LSA. The time averaged solution was obtained from DAS of the rigid airfoil [26]. Quality of time averaged solution as a base flow was evaluated by LSA without any perturbation and the deviation from its initial state was checked.…”
Section: Linear Stability Analysismentioning
confidence: 99%