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Design considerations for composite fuselage structure of commercial transport aircraftThe structural, manufacturing, and service and environmental considerations that could impact the design of composite fuselage structure for commercial transport aircraft application were explored. The severity of these considerations was assessed and the principal design drivers delineated. Technical issues and potential problem areas which must be resolved before sufficient confidence is established to commit to composite materials were defined. The key issues considered are: definition of composite fuselage design specifications, damage tolerance, and crashworthiness.
Document ID
19810013888
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Davis, G. W.
(Lockheed-California Co. Burbank, CA, United States)
Sakata, I. F.
(Lockheed-California Co. Burbank, CA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1981
Publication Information
Publisher: NASA. Langley Research Center
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-159296
LR-29540
Accession Number
81N22419
Funding Number(s)
CONTRACT_GRANT: NAS1-15949
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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