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Development of Computer Models for the Assessment of Foreign Body Impact Events on Composite StructuresThe objective of this project was to model the 5-3/4 inch pressure vessels used on the NASA RTOP program in an attempt to learn more about how impact damage forms and what are the residual effects of the resulting damage. A global-local finite element model was developed for the bottle and the states of stress in the bottles were determined down to the constituent level. The experimental data that was generated on the NASA RTOP program was not in a form that enabled the model developed under this grant to be correlated with the experimental data. As a result of this exercise it is recommended that an experimental program be designed using statistical design of experiment techniques to generate data that can be used to isolate the phenomenon that control the formation of impact damage. This data should include residual property determinations so that models for post impact structural integrity can be developed. It is also recommended that the global-local methodology be integrated directly into the finite element code. This will require considerable code development.
Document ID
19970036054
Acquisition Source
Marshall Space Flight Center
Document Type
Contractor Report (CR)
Authors
Bucinell, Ronald B.
(Union Coll. Schenectady, NY United States)
Date Acquired
September 6, 2013
Publication Date
January 2, 1997
Subject Category
Composite Materials
Report/Patent Number
NASA/CR-97-205859
NAS 1.26:205859
Report Number: NASA/CR-97-205859
Report Number: NAS 1.26:205859
Accession Number
97N30424
Funding Number(s)
CONTRACT_GRANT: NAG8-1144
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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