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An Analysis Technique/Automated Tool for Comparing and Tracking Analysis Modes of Different Finite Element ModelsAn analysis technique was developed to compare and track mode shapes for different Finite Element Models. The technique may be applied to a variety of structural dynamics analyses, including model reduction validation (comparing unreduced and reduced models), mode tracking for various parametric analyses (e.g., launch vehicle model dispersion analysis to identify sensitivities to modal gain for Guidance, Navigation, and Control), comparing models of different mesh fidelity (e.g., a coarse model for a preliminary analysis compared to a higher-fidelity model for a detailed analysis) and mode tracking for a structure with properties that change over time (e.g., a launch vehicle from liftoff through end-of-burn, with propellant being expended during the flight). Mode shapes for different models are compared and tracked using several numerical indicators, including traditional Cross-Orthogonality and Modal Assurance Criteria approaches, as well as numerical indicators obtained by comparing modal strain energy and kinetic energy distributions. This analysis technique has been used to reliably identify correlated mode shapes for complex Finite Element Models that would otherwise be difficult to compare using traditional techniques. This improved approach also utilizes an adaptive mode tracking algorithm that allows for automated tracking when working with complex models and/or comparing a large group of models.
Document ID
20120014370
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Towner, Robert L.
(Jacobs Technologies Engineering Science Contract Group Huntsville, AL, United States)
Band, Jonathan L.
(Jacobs Technologies Engineering Science Contract Group Huntsville, AL, United States)
Date Acquired
August 26, 2013
Publication Date
April 23, 2012
Subject Category
Structural Mechanics
Report/Patent Number
M11-0857
M12-1683
Report Number: M11-0857
Report Number: M12-1683
Meeting Information
Meeting: 53rd AIAA Structures, Structural Dynamics and Materials Conference
Location: Honolulu, HI
Country: United States
Start Date: April 23, 2012
End Date: April 26, 2012
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNM05AB50C
Distribution Limits
Public
Copyright
Public Use Permitted.
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