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INTERACTION OF A SLOT-TONE WITH A PIPE
Alexis Billon, Vincent Valeau and Anas Sakout L.E.P.T.A.B., University of La Rochelle, France
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Summary Experimental apparatus
Overview of the operating range of the self-sustained tones Evolution of the slot-tone with the jet velocity and the system geometry Identification of the amplified instability Comparison of the acoustic fields within and outside the pipe Conclusion
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Experimental apparatus
Length parameter: Fundamental frequency of the tones
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Overview of the self-sustained tones
Typical pressure spectrum f0 2f0 f0/2 f0+f0/2 Operating range of the self-sustained tones: Velocity : from Re0=2400 Geometric : 1.1<L/H<7.5 S.P.L.max = 115 dB
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Influence of the plate distance (Re0=11.104)
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Calculation of the shear-layer natural frequency
Michalke’s formula : Where : fn = 1350 Hz Calculated frequency : Conclusion : same order of magnitude than the self-sustained tones
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Influence of the jet velocity (L/H=3.0)
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Comparison of the radiated acoustic field with the acoustic field inside the duct
Coherence Radiated acoustic field
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Comparison of the radiated acoustic field with the acoustic field inside the duct
Coherence Radiated acoustic field
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Conclusion Strong self-sustained tones occur over Re0=2400 and 1.1<L/H<7.5 The self-sustained tones are the result of the shear-layer instabilities Below Re0~7000, the inner and the outer acoustic fields of the duct are weackly coupled. The hydrodynamic feedback is dominant. Above Re0~7000, the pipe acoustic field reinforces and controls the self-sustained tones. The acoustic feedback is dominant.
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