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Using Response Surface Methods to Correlate the Modal Test of an Inflatable Test ArticleThis paper presents a practical application of response surface methods (RSM) to correlate a finite element model of a structural modal test. The test article is a quasi‐cylindrical inflatable structure which primarily consists of a fabric weave, with an internal bladder and metallic bulkheads on either end. To mitigate model size, the fabric weave was simplified by representing it with shell elements. The task at hand is to represent the material behavior of the weave. The success of the model correlation is measured by comparing the four major modal frequencies of the analysis model to the four major modal frequencies of the test article. Given that only individual strap material properties were provided and material properties of the overall weave were not available, defining the material properties of the finite element model became very complex. First it was necessary to determine which material properties (modulus of elasticity in the hoop and longitudinal directions, shear modulus, Poisson's ratio, etc.) affected the modal frequencies. Then a Latin Hypercube of the parameter space was created to form an efficiently distributed finite case set. Each case was then analyzed with the results input into RSM. In the resulting response surface it was possible to see how each material parameter affected the modal frequencies of the analysis model. If the modal frequencies of the analysis model and its corresponding parameters match the test with acceptable accuracy, it can be said that the model correlation is successful.
Document ID
20140000332
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Gupta, Anju
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
January 22, 2014
Publication Date
July 16, 2013
Subject Category
Structural Mechanics
Report/Patent Number
JSC-CN-28997
Report Number: JSC-CN-28997
Meeting Information
Meeting: SLaMS Young Professional Forum
Location: Hampton, VA
Country: United States
Start Date: July 16, 2013
End Date: July 18, 2013
Sponsors: NASA Langley Research Center
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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