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Materials and structures/ACEELight weight composites made from graphite fibers, glass, or man made materials held in an epoxy matrix, and their application to airframe design are reviewed. The Aircraft Energy Efficiency program is discussed. Characteristics of composites, acceptable risks, building parts and confidence, and aeroelastic tailoring are considered.
Document ID
19820017366
Acquisition Source
Legacy CDMS
Document Type
Other - Other
Date Acquired
September 4, 2013
Publication Date
January 1, 1981
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-FACTS-117/8-81
Accession Number
82N25242
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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