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Composite fuselage technologyThe overall objective is to identify and understand, via directed experimentation and analysis, the mechanisms which control the structural behavior of fuselages in their response to damage (resistance, tolerance, and arrest). A further objective is to develop straightforward design methodologies which can be employed by structural designers in preliminary design stages to make intelligent choices concerning the material, layup, and structural configuration so that a more efficient structure with structural integrity can be designed and built.
Document ID
19910004133
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Graves, Michael J.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Lagace, Paul A.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1990
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-187658
TELAC-90-19
NAS 1.26:187658
Report Number: NASA-CR-187658
Report Number: TELAC-90-19
Report Number: NAS 1.26:187658
Accession Number
91N13446
Funding Number(s)
CONTRACT_GRANT: NAG1-991
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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