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Advanced composite vertical fin for L-1011 aircraftThe structural box of the L-1011 vertical fin was redesigned using advanced composite materials. The box was fabricated and ground tested to verify the structural integrity. This report summarizes the complete program starting with the design and analysis and proceeds through the process development ancillary test program production readiness verification testing, fabrication of the full-scale fin boxes and the full-scale ground testing. The program showed that advanced composites can economically and effectively be used in the design and fabrication of medium primary structures for commercial aircraft. Static-strength variability was demonstrated to be comparable to metal structures and the long term durability of advanced composite components was demonstrated.
Document ID
19870019184
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jackson, A. C.
(Lockheed-California Co. Burbank, CA, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1984
Publication Information
Publisher: NASA
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-3816
NAS 1.26:3816
Report Number: NASA-CR-3816
Report Number: NAS 1.26:3816
Accession Number
87N28617
Funding Number(s)
CONTRACT_GRANT: NAS1-14000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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