2018 AIAA Aerospace Sciences Meeting 2018
DOI: 10.2514/6.2018-0758
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Experimental Slat Noise Assessment Through Phased Array and Hot-Film Anemometry Measurements

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Cited by 4 publications
(7 citation statements)
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“…Between this vortex and the undisturbed flow, a free and unstable shear layer develops originating at the cusp and impacting the surface of the cove ( Figure 6). Choudhari and Khorrami (2006) These instabilities that lead to slat noise are probably generated in the shear layer of the slat (PEREIRA et al, 2018). Khorrami (2003) demonstrated that this shear layer is an amplifier of low and medium frequency disturbances.…”
Section: Flap Noisementioning
confidence: 99%
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“…Between this vortex and the undisturbed flow, a free and unstable shear layer develops originating at the cusp and impacting the surface of the cove ( Figure 6). Choudhari and Khorrami (2006) These instabilities that lead to slat noise are probably generated in the shear layer of the slat (PEREIRA et al, 2018). Khorrami (2003) demonstrated that this shear layer is an amplifier of low and medium frequency disturbances.…”
Section: Flap Noisementioning
confidence: 99%
“…Choudhari and Khorrami (2007) also suggests that an optimal strategy to mitigate broadband slat noise should target the shear layer reattachment region, in order to reduce the amplitude of surface pressure fluctuations. Pereira et al (2018) determined the location of the shear layer reattachment point in the slat cove through the coherence between two consecutive hot film sensors, finding that the reattachment position moves slowly toward the slat trailing edge with increasing angle of attack. The model in which Pereira et al (2018) performed their measurements is the same one that will be used in the experiments of the research presented here.…”
Section: Flap Noisementioning
confidence: 99%
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