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Through-the Thickness(R) braided composites for aircraft applicationsMaterial and structural specimens of Through-the-Thickness(R) braided textile composites were tested in a variety of experiments. The results have demonstrated that the preform architecture provides significant payoffs in damage tolerance, delamination resistance, and attachment strength. This paper describes the braiding process, surveys the experimental data base, and illustrates the application of three dimensional braiding in aircraft structures.
Document ID
19950021852
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brown, Richard T.
(Atlantic Research Corp. Alexandria, VA, 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 3
Subject Category
Composite Materials
Accession Number
95N28273
Distribution Limits
Public
Copyright
Public Use Permitted.
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