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Advanced composites research and development for transport aircraftThis paper highlights past experiences, lessons learned, state-of-the-art and current research activities directed at providing an integrated 'affordable' data base for composite structures. Composite secondary and empennage structures are in production on several transport aircraft. The weight reduction potential of composite structures is well documented. However, the cost to develop and produce composite structures remains the major barrier to increased application of this technology to transport aircraft. Specific technology items that are being developed under the NASA Advanced Composites Technology Program are described. Materials, design concepts, structural mechanics methodology and manufacturing processes and equipment are under development or are emerging that are expected to lead to an integrated 'affordable' data base. Technology verification for the next decade is expected to require fabrication and testing of full-scale wing-box and fuselage-section components before certificatiaon can occur and production commitments can be made.
Document ID
19910039680
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Davis, John G., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Starnes, James H., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Johnston, Norman J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1990
Subject Category
Aircraft Design, Testing And Performance
Accession Number
91A24303
Distribution Limits
Public
Copyright
Other

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