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Correlation Results for a Mass Loaded Vehicle Panel Test Article Finite Element Models and Modal Survey TestsHigh-fidelity Finite Element Models (FEMs) were developed to support a recent test program at Marshall Space Flight Center (MSFC). The FEMs correspond to test articles used for a series of acoustic tests. Modal survey tests were used to validate the FEMs for five acoustic tests (a bare panel and four different mass-loaded panel configurations). An additional modal survey test was performed on the empty test fixture (orthogrid panel mounting fixture, between the reverb and anechoic chambers). Modal survey tests were used to test-validate the dynamic characteristics of FEMs used for acoustic test excitation. Modal survey testing and subsequent model correlation has validated the natural frequencies and mode shapes of the FEMs. The modal survey test results provide a basis for the analysis models used for acoustic loading response test and analysis comparisons
Document ID
20120014454
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Maasha, Rumaasha
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Towner, Robert L.
(Jacobs Engineering Group, Inc. Huntsville, AL, United States)
Date Acquired
August 26, 2013
Publication Date
April 23, 2012
Subject Category
Acoustics
Report/Patent Number
M12-1664
M11-0920
Report Number: M12-1664
Report Number: M11-0920
Meeting Information
Meeting: 53rd Structures, Structural Dynamics, and Materials Conference (SDM)
Location: Honolulu, HI
Country: United States
Start Date: April 23, 2012
End Date: April 26, 2012
Sponsors: American Helicopter Society, Inc., American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers
Distribution Limits
Public
Copyright
Public Use Permitted.
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