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Composite structural materialsThe promise of filamentary composite materials, whose development may be considered as entering its second generation, continues to generate intense interest and applications activity. Fiber reinforced composite materials offer substantially improved performance and potentially lower costs for aerospace hardware. Much progress has been achieved since the initial developments in the mid 1960's. Rather limited applications to primary aircraft structure have been made, however, mainly in a material-substitution mode on military aircraft, except for a few experiments currently underway on large passenger airplanes in commercial operation. To fulfill the promise of composite materials completely requires a strong technology base. NASA and AFOSR recognize the present state of the art to be such that to fully exploit composites in sophisticated aerospace structures, the technology base must be improved. This, in turn, calls for expanding fundamental knowledge and the means by which it can be successfully applied in design and manufacture.
Document ID
19830009326
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ansell, G. S.
(Rensselaer Polytechnic Inst. Troy, NY, United States)
Loewy, R. G.
(Rensselaer Polytechnic Inst. Troy, NY, United States)
Wiberley, S. E.
(Rensselaer Polytechnic Inst. Troy, NY, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1982
Subject Category
Composite Materials
Report/Patent Number
NAS 1.26:169859
NASA-CR-169859
SAR-43
Report Number: NAS 1.26:169859
Report Number: NASA-CR-169859
Report Number: SAR-43
Accession Number
83N17597
Funding Number(s)
CONTRACT_GRANT: NGL-33-018-003
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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