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Stress analysis and buckling of J-stiffened graphite-epoxy panelA graphite epoxy shear panel with bonded on J stiffeners was investigated. The panel, loaded to buckling in a picture frame shear test is described. Two finite element models, each of which included the doubler material bonded to the panel skin under the stiffeners and at the panel edges, were used to make a stress analysis of the panel. The shear load distributions in the panel from two commonly used boundary conditions, applied shear load and applied displacement, were compared with the results from one of the finite element models that included the picture frame test fixture.
Document ID
19800010153
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Davis, R. C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1980
Subject Category
Structural Mechanics
Report/Patent Number
L-13256
NASA-TP-1607
Report Number: L-13256
Report Number: NASA-TP-1607
Accession Number
80N18427
Funding Number(s)
PROJECT: RTOP 506-17-23-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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