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Experimental behavior of graphite-epoxy Y-stiffened specimens loaded in compressionAn experimental investigation of the behavior of graphite-epoxy Y-stiffened specimens loaded in compression is presented. Experimental results are presented for element specimens with a single stiffener and for panel specimens with three stiffeners. Response and failure characteristics of the specimens are described. Effects of impact damage on structural response for both specimen configurations are also presented. Experimental results indicate that impact location may significantly affect the residual strength of the Y-stiffened specimens. The failure results indicate that the critical failure mode is buckling of the stiffener webs for Y-stiffened element specimens and buckling of the stiffener webs and other stiffener blades for the Y-stiffened panel specimens.
Document ID
19920013872
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Sydow, P. Daniel
(NASA Langley Research Center Hampton, VA, United States)
Shuart, Mark J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1992
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TP-3171
NAS 1.60:3171
L-16918
Report Number: NASA-TP-3171
Report Number: NAS 1.60:3171
Report Number: L-16918
Accession Number
92N23115
Funding Number(s)
PROJECT: RTOP 505-63-50-08
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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