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Substructure Versus Property-Level Dispersed Modes CalculationThis paper calculates the effect of perturbed finite element mass and stiffness values on the eigenvectors and eigenvalues of the finite element model. The structure is perturbed in two ways: at the "subelement" level and at the material property level. In the subelement eigenvalue uncertainty analysis the mass and stiffness of each subelement is perturbed by a factor before being assembled into the global matrices. In the property-level eigenvalue uncertainty analysis all material density and stiffness parameters of the structure are perturbed modified prior to the eigenvalue analysis. The eigenvalue and eigenvector dispersions of each analysis (subelement and property-level) are also calculated using an analytical sensitivity approximation. Two structural models are used to compare these methods: a cantilevered beam model, and a model of the Space Launch System. For each structural model it is shown how well the analytical sensitivity modes approximate the exact modes when the uncertainties are applied at the subelement level and at the property level.
Document ID
20160001821
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Stewart, Eric C.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Peck, Jeff A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Bush, T. Jason
(TriVector Services, Inc. Huntsville, AL, United States)
Fulcher, Clay W.
(Jacobs Engineering Group, Inc. Huntsville, AL, United States)
Date Acquired
February 16, 2016
Publication Date
January 4, 2016
Subject Category
Structural Mechanics
Spacecraft Design, Testing And Performance
Report/Patent Number
M16-5016
Report Number: M16-5016
Meeting Information
Meeting: AIAA SciTech 2016
Location: San Diego, CA
Country: United States
Start Date: January 4, 2016
End Date: January 8, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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