NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A Patch Density Recommendation based on Convergence Studies for Vehicle Panel Vibration Response resulting from Excitation by a Diffuse Acoustic FieldProducing fluid structural interaction estimates of 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. It is a useful practice to simulate the spatial correlation of the applied pressure field over a 2d surface using a matrix of small patch area regions on a finite element model (FEM). Use of a fitted function for the spatial correlation between patch centers can result in an error 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. Several patch density assumptions to approximate the fitted spatial correlation function are first evaluated using both qualitative and quantitative illustrations. The actual response of a typical vehicle panel system FEM is then examined in a convergence study where the patch density assumptions are varied over the same model. The convergence study results illustrate the impacts possible from a poor choice of patch density on the analytical response estimate. The fitted correlation function used in this study represents a diffuse acoustic field (DAF) excitation of the panel to produce vibration response.
Document ID
20130013895
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)
Waldon, James
(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
M13-2497
Meeting Information
Meeting: 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference and Co-located Events
Location: Boston, MA
Country: United States
Start Date: April 8, 2011
End Date: April 11, 2011
Sponsors: Department of the Army, NASA Headquarters, Department of the Navy, Department of the Air Force
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available