NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Interlaminar fracture of compositesFracture mechanics has been found to be a useful tool for understanding composite delamination. Analyses for calculating strain energy release rates associated with delamination growth have been developed. These analyses successfully characterized delamination onset and growth for particular sources of delamination. Low velocity impact has been found to be the most severe source of composite delamination. A variety of test methods for measuring interlaminar fracture toughness are being developed to identify new composite materials with enhanced delamination resistance.
Document ID
19840019766
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Obrien, T. K.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1984
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-85768
NAS 1.15:85768
USAAVSCOM-TR-84-B-2
Report Number: NASA-TM-85768
Report Number: NAS 1.15:85768
Report Number: USAAVSCOM-TR-84-B-2
Accession Number
84N27835
Funding Number(s)
PROJECT: DA PROJ. 1L1-61102-AH-45
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available