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Modelling Unsteady Wall Pressures Beneath Turbulent Boundary LayersAs a structural entity of turbulence, hairpin vortices are believed to play a major role in developing and sustaining the turbulence process in the near wall region of turbulent boundary layers and may be regarded as the simplest conceptual model that can account for the essential features of the wall pressure fluctuations. In this work we focus on fully developed typical hairpin vortices and estimate the associated surface pressure distributions and their corresponding spectra. On the basis of the attached eddy model, we develop a representation of the overall surface pressure spectra in terms of the eddy size distribution. Instantaneous wavenumber spectra and spatial correlations are readily derivable from this representation. The model is validated by comparison of predicted wavenumber spectra and cross-correlations with existing emperical models and experimental data.
Document ID
20040074207
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Ahn, B-K.
(Cambridge Univ. Cambridge, United Kingdom)
Graham, W. R.
(Cambridge Univ. Cambridge, United Kingdom)
Rizzi, S. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
May 3, 2004
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA Paper 2004-2849
Report Number: AIAA Paper 2004-2849
Meeting Information
Meeting: 10th AIAA/CEAS Aeroacoustics Conference
Location: Manchester
Country: United Kingdom
Start Date: May 10, 2004
End Date: May 12, 2004
Sponsors: Confederation of European Aerospace Societies, American Inst. of Aeronautics and Astronautics
Funding Number(s)
OTHER: 781-20-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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