25th AIAA/CEAS Aeroacoustics Conference 2019
DOI: 10.2514/6.2019-2651
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Uniform Suction for the Reduction of the Trailing-Edge Noise

Abstract: Uniform inclined suction from a spanwise slot is applied upstream of a trailing edge on a zero pressure gradient flat plate with the aim of reducing trailing edge noise. The effects of the flow treatment on the turbulence statistics are experimentally investigated downstream of the flow control section using hot-wire anemometry. Surface pressure measurements from flush-mounted microphones are used to estimate the far-field trailing edge noise. The area of the flow control is kept constant, while the flow sucti… Show more

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“…Increasing flow control severity would increase the viscous region while decreasing the logarithmic region. The logarithmic region disappears when flow control severity is greater than 6 [63]. The highest noise reduction of about 5dB is achieved at a flow control severity of 6 and the suction angle of 70°.…”
Section: Noise Controlmentioning
confidence: 95%
“…Increasing flow control severity would increase the viscous region while decreasing the logarithmic region. The logarithmic region disappears when flow control severity is greater than 6 [63]. The highest noise reduction of about 5dB is achieved at a flow control severity of 6 and the suction angle of 70°.…”
Section: Noise Controlmentioning
confidence: 95%