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The Influence of Restraint Systems on Panel BehaviorWhen a panel is tested in uniaxial compression in a test machine, the boundary conditions are not quite the same as they would be if it were part of a complete structure. A restraint system may be used to simulate conditions found in a complete vehicle. Quantifying the quality of the restraint with only point-measurement devices can leave an inadequate characterization of the out-of-plane behavior. However, today s full-field displacement monitoring techniques allow for much more accurate views of the global panel deformation and strain, and therefore allow for a better understanding of panel behavior. In the current study, the behavior of a hat-stiffened and two rod-stiffened carbon-epoxy panels is considered. Panels were approximately 2 meters tall and 0.76 to 1.06 m wide. Unloaded edges were supported by knife edges and stiffeners were attached to a support structure at selected locations to restrain out-of-plane motion. A comparison is made between test results based on full-field measurements and analyses based on assumptions of boundary conditions of a completely rigid edge restraint and the absence of any edge restraint. Results indicate that motion at the restrained edges must be considered to obtain accurate test-analysis correlation.
Document ID
20110012873
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Jegley, Dawn C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
June 13, 2011
Subject Category
Composite Materials
Report/Patent Number
NF1676L-11408
Report Number: NF1676L-11408
Meeting Information
Meeting: SEM Annual Conference and Exposition on Experimental and Applied Mechanics
Location: Uncasville, CT
Country: United States
Start Date: June 13, 2011
End Date: June 15, 2011
Funding Number(s)
WBS: WBS 699959.02.08.07.02.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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