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Advanced textile applications for primary aircraft structuresAdvanced composite primary structural concepts have been evaluated for low cost, damage tolerant structures. Development of advanced textile preforms for fuselage structural applications with resin transfer molding and powder epoxy material is now under development.
Document ID
19950022055
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jackson, Anthony C. (Lockheed Aeronautical Systems Co. Marietta, GA, United States)
Barrie, Ronald E. (Lockheed Aeronautical Systems Co. Marietta, GA, United States)
Shah, Bharat M. (Lockheed Aeronautical Systems Co. Marietta, GA, United States)
Shukla, Jay G. (Lockheed Aeronautical Systems Co. Marietta, GA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1992
Publication Information
Publication: FAA, Ninth DOD(NASA)FAA Conference on Fibrous Composites in Structural Design, Volume 2
Subject Category
Aircraft Design, Testing And Performance
Accession Number
95N28476
Funding Number(s)
CONTRACT_GRANT: NAS1-18888
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19950021999Collected WorksNinth DOD/NASA/FAA Conference on Fibrous Composites in Structural Design, volume 1
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