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The transmission of turbulent boundary layer unsteady pressure and shear stress through a viscoelastic layer
Affiliation:1. Tsinghua National Laboratory for Information Science and Technology (TNList) and Department of Automation, Tsinghua University, Beijing 100084, PR China;2. College of Electrical Engineering and Automation, Shandong University of Science and Technology, Qingdao 266590, PR China;1. Department of Aerospace Engineering, Indian Institute of Science, Bangalore 560012, India;2. Pratt & Whitney Canada, Mississauga, Ontario L5T 1J3, Canada;3. Indian Institute of Petroleum, Dehradun 248005, India;1. Department of Transport & Planning, Faculty of Civil Engineering and Geosciences, Delft University of Technology, 2628 BX Delft, The Netherlands;2. Department of Air Transport and Operations, Faculty of Aerospace Engineering, Delft University of Technology, Kluyverweg 1, 2629 HS Delft, The Netherlands
Abstract:The transmission of unsteady pressure and shear stress, generated by a turbulent boundary layer in water, through a viscoelastic layer backed by a rigid plate is investigated. Analytical models are used to estimate the unsteady pressure and shear stress from 10 to 1000 Hz for a flat plate boundary layer with zero pressure gradient. Additionally, models for the transfer of the unsteady pressures and shear stress through the viscoelastic layer are developed. The models are used to predict the unsteady pressure fluctuations, or flow noise, which would be seen by a finite size sensor embedded under the elastomer layer. The unsteady pressure levels are found to be 20 dB greater than the unsteady shear stress levels across all frequency ranges computed, in agreement with recent measurements. The unsteady pressure transfer functions have a peak at the shear wavenumber and are larger than the shear stress transfer magnitudes from 10 to 50 Hz. The unsteady shear stress transfer functions have a peak at the acoustic wavenumber and are larger than the pressure transfer magnitudes from 50 to 1000 Hz. Over the frequency range examined, the unsteady pressures were found to be the dominant contributor to the sensor flow noise due to the considerably larger magnitude of the unsteady pressures on the top of the viscoelastic layer.
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