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Transition from glass to graphite in manufacture of composite aircraft structureThe transition from fiberglass reinforced plastic composites to graphite reinforced plastic composites is described. Structural fiberglass design and manufacturing background are summarized. How this experience provides a technology base for moving into graphite composite secondary structure and then to composite primary structure is considered. The technical requirements that must be fulfilled in the transition from glass to graphite composite structure are also included.
Document ID
19780019122
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Buffum, H. E.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Thompson, V. S.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
August 9, 2013
Publication Date
June 1, 1978
Publication Information
Publication: NASA. Langley Res. Center CTOL Transport Technol., 1978
Subject Category
Aircraft Design, Testing And Performance
Accession Number
78N27065
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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