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ACEE composite structures technologyThe NASA Aircraft Energy Efficiency (ACEE) Composite Primary Aircraft Structures Program has made significant progress in the development of technology for advanced composites in commercial aircraft. Commercial airframe manufacturers have demonstrated technology readiness and cost effectiveness of advanced composites for secondary and medium primary components and have initiated a concerted program to develop the data base required for efficient application to safety-of-flight wing and fuselage structures. Oral presentations were compiled into five papers. Topics addressed include: damage tolerance and failsafe testing of composite vertical stabilizer; optimization of composite multi-row bolted joints; large wing joint demonstation components; and joints and cutouts in fuselage structure.
Document ID
19870019180
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Klotzsche, M.
(McDonnell-Douglas Corp. Long Beach, CA, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1984
Subject Category
Composite Materials
Report/Patent Number
NAS 1.26:172359
NASA-CR-172359
Report Number: NAS 1.26:172359
Report Number: NASA-CR-172359
Accession Number
87N28613
Funding Number(s)
CONTRACT_GRANT: NAS1-17701
PROJECT: RTOP 534-06-13
CONTRACT_GRANT: NAS1-16857
CONTRACT_GRANT: NAS1-14869
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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