NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Delamination, durability, and damage tolerance of laminated composite materialsDurability and damage tolerance may have different connotations to people from different industries and with different backgrounds. Damage tolerance always refers to a safety of flight issue where the structure must be able to sustain design limit loads in the presence of damage and return to base safely. Durability, on the other hand, is an economic issue where the structure must be able to survive a certain life under load before the initiation of observable damage. Delamination is typically the observable damage mechanism that is of concern for durability, and the growth and accumulation of delaminations through the laminate thickness is often the sequence of events that leads to failure and the loss of structural integrity.
Document ID
19940018149
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Obrien, T. Kevin
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1993
Publication Information
Publication: Computational Methods for Failure Analysis and Life Prediction
Subject Category
Composite Materials
Accession Number
94N22622
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available