Light 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.
Materials and structures/ACEE
1981-01-01
Miscellaneous
No indication
English
NTIS | 1981
ACEE composite structures technology
NTRS | 1984
|ACEE composite structures technology
NTRS | 1984
|NTIS | 1981
NTRS | 1978
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