NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Failure characteristics of graphite-epoxy structural components loaded in compressionFailure characteristics of compressively loaded graphite-epoxy components are described. Experimental results for both strength-critical laminates and structural components with postbuckling strength are presented. Effects of low speed impact damage and circular holes on compressive strength are discussed. Delamination and shear crippling failure mechanisms that limit the performance of strength-critical laminates are described. Transverse shear and skin-stiffener separation failure mechanisms that limit the performance of components with postbuckling strength are also described. The influence of matrix properties on compressive strength improvements for impact damaged laminates is discussed. Experimental data and results from a failure analysis for strength-critical laminates with cutouts are discussed and compared with impact damage results. Typical postbuckling test results are compared with analytical predictions.
Document ID
19830003904
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Starnes, J. H., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Williams, J. G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1982
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:84552
NASA-TM-84552
Report Number: NAS 1.15:84552
Report Number: NASA-TM-84552
Meeting Information
Meeting: IUTAM Symp. on Mech. of Composite Mater.
Location: Blacksburg, VA
Country: United States
Start Date: August 16, 1982
End Date: August 19, 1982
Accession Number
83N12174
Funding Number(s)
PROJECT: RTOP 505-33-33-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available