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Application of composites to the selective reinforcement of metallic aerospace structuresThe use of composite materials to selectively reinforce metallic structures provides a low-cost way to reduce weight and a means of minimizing the risks usually associated with the introduction of new materials. An overview is presented of the NASA Langley Research Center programs to identify the advantages and to develop the potential of the selective reinforcement approach to the use of composites. These programs have shown that selective reinforcement provides excellent strength and stiffness improvements to metallic structures. Significant weight savings can be obtained in a cost effective manner. Flight service programs which have been initiated to validate further the merits of selective reinforcement are described.
Document ID
19740012540
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brooks, W. A., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Mathauser, E. E.
(NASA Langley Research Center Hampton, VA, United States)
Pride, R. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1972
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-71939
Report Number: NASA-TM-X-71939
Meeting Information
Meeting: AGARD Symp. on Impact of Composite Mater. on Aerospace Vehicles and Propulsion Systems
Location: Toulouse
Start Date: September 20, 1972
End Date: September 22, 1972
Accession Number
74N20653
Funding Number(s)
PROJECT: RTOP 501-22-03-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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