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Structural Efficiencies Of Fluted-Core Graphite/Epoxy PanelsReport discusses one concept providing alternative to some aluminum structural components of wings: fluted core panels made of graphite/epoxy material. Includes description of structural-efficiency study of fluted-core sandwich panels of two different configurations. Results of study compared with results of similar study of conventional aluminum panels and blade-stiffened graphite/epoxy panels.
Document ID
19930000429
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Jegley, Dawn C. (NASA Langley Research Center, Hampton, VA.)
Date Acquired
August 16, 2013
Publication Date
July 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 7
ISSN: 0145-319X
Subject Category
Materials
Report/Patent Number
LAR-14539
Report Number: LAR-14539
ISSN: 0145-319X
Accession Number
93B10429
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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