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Hole interaction and load introduction effects for compression-loaded laminates with holesThe effects of hole interaction and load introduction for (+ or - 30/90) sub 8 (s) and (+ or - 45) sub 12 (s) laminates with holes was conducted. A hole interaction region was identified in some specimens, and this region was ineffective for carrying load. The membrane stiffness of a specimen with a hole interaction region is less than the membrane stiffness of a similar specimen without a hole interaction region. A load introduction effect that occurs on the sublaminate level was also observed. This effect can cause a nonuniform load diffusion into the interior of the specimen.
Document ID
19840024365
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Shuart, M. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1984
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:86287
NASA-TM-86287
Report Number: NAS 1.15:86287
Report Number: NASA-TM-86287
Meeting Information
Meeting: Intern. Symp. on Composites: Mater. and Eng.
Location: Newark, DE
Country: United States
Start Date: September 24, 1984
End Date: September 28, 1984
Accession Number
84N32435
Funding Number(s)
PROJECT: RTOP 505-33-33
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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