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Composite Stress Rupture: A New Reliability Model Based on Strength DecayA model is proposed to estimate reliability for stress rupture of composite overwrap pressure vessels (COPVs) and similar composite structures. This new reliability model is generated by assuming a strength degradation (or decay) over time. The model suggests that most of the strength decay occurs late in life. The strength decay model will be shown to predict a response similar to that predicted by a traditional reliability model for stress rupture based on tests at a single stress level. In addition, the model predicts that even though there is strength decay due to proof loading, a significant overall increase in reliability is gained by eliminating any weak vessels, which would fail early. The model predicts that there should be significant periods of safe life following proof loading, because time is required for the strength to decay from the proof stress level to the subsequent loading level. Suggestions for testing the strength decay reliability model have been made. If the strength decay reliability model predictions are shown through testing to be accurate, COPVs may be designed to carry a higher level of stress than is currently allowed, which will enable the production of lighter structures
Document ID
20120008181
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Reeder, James R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
April 1, 2012
Subject Category
Composite Materials
Report/Patent Number
NF1676L-14234
NASA/TM-2012-217566
L-20122
Report Number: NF1676L-14234
Report Number: NASA/TM-2012-217566
Report Number: L-20122
Funding Number(s)
WBS: WBS 869021-03-07.02.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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