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Evaluation of a Linear Cumulative Damage Failure Model for Epoxy AdhesiveRecently a significant amount of work has been conducted to provide more complex and accurate material models for use in the evaluation of adhesive bondlines. Some of this has been prompted by recent studies into the effects of residual stresses on the integrity of bondlines. Several techniques have been developed for the analysis of bondline residual stresses. Key to these analyses is the criterion that is used for predicting failure. Residual stress loading of an adhesive bondline can occur over the life of the component. For many bonded systems, this can be several years. It is impractical to directly characterize failure of adhesive bondlines under a constant load for several years. Therefore, alternative approaches for predictions of bondline failures are required. In the past, cumulative damage failure models have been developed. These models have ranged from very simple to very complex. This paper documents the generation and evaluation of some of the most simple linear damage accumulation tensile failure models for an epoxy adhesive. This paper shows how several variations on the failure model were generated and presents an evaluation of the accuracy of these failure models in predicting creep failure of the adhesive. The paper shows that a simple failure model can be generated from short-term failure data for accurate predictions of long-term adhesive performance.
Document ID
20020018164
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Richardson, David E.
(Thiokol Propulsion Brigham City, UT United States)
Batista-Rodriquez, Alicia
(Thiokol Propulsion Brigham City, UT United States)
Macon, David
(Thiokol Propulsion Brigham City, UT United States)
Totman, Peter
(Thiokol Propulsion Brigham City, UT United States)
McCool, Alex
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Quality Assurance And Reliability
Report/Patent Number
AIAA Paper 2001-6123
Report Number: AIAA Paper 2001-6123
Meeting Information
Meeting: AIAA Joint Propulsion Conference
Location: Salt Lake City, UT
Country: United States
Start Date: July 8, 2001
End Date: July 11, 2001
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NAS8-97238
Distribution Limits
Public
Copyright
Public Use Permitted.
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