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A Patch Density Recommendation based on Convergence Studies for Vehicle Panel Vibration Response resulting from Excitation by a Diffuse Acoustic FieldFluid structural interaction problems that estimate panel vibration from an applied pressure field excitation are quite dependent on the spatial correlation of the pressure field. There is a danger of either over estimating a low frequency response or under predicting broad band panel response in the more modally dense bands if the pressure field spatial correlation is not accounted for adequately. Even when the analyst elects to use a fitted function for the spatial correlation an error may be introduced if the choice of patch density is not fine enough to represent the more continuous spatial correlation function throughout the intended frequency range of interest. Both qualitative and quantitative illustrations evaluating the adequacy of different patch density assumptions to approximate the fitted spatial correlation function are provided. The actual response of a typical vehicle panel system is then evaluated in a convergence study where the patch density assumptions are varied over the same finite element model. The convergence study results are presented illustrating the impact resulting from a poor choice of patch density. The fitted correlation function used in this study represents a Diffuse Acoustic Field (DAF) excitation of the panel to produce vibration response.
Document ID
20130013856
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Smith, Andrew
(NASA Marshall Space Flight Center Huntsville, AL, United States)
LaVerde, Bruce
(Engineering Research and Consulting, Inc. Huntsville, AL, United States)
Jones, Douglas
(Jacobs Engineering Group, Inc. Huntsville, AL, United States)
Towner, Robert
(Jacobs Engineering Group, Inc. Huntsville, AL, United States)
Hunt, Ron
(Bevilacqua Research Corp. Huntsville, AL, United States)
Date Acquired
August 27, 2013
Publication Date
April 8, 2013
Subject Category
Acoustics
Report/Patent Number
M12-2090
Meeting Information
Meeting: 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Location: Boston, MA
Start Date: April 8, 2013
End Date: April 11, 2013
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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