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Design properties of randomly reinforced fiber compositesThe pseudoisotropic-laminate analogy is used in conjunction with fiber composite micro- and macromechanics to predict the thermal and mechanical properties of planar randomly reinforced fiber composites (PRRFC). Theoretical results are presented for boron/aluminum, boron/epoxy, Thornel-50/epoxy, and S-glass/epoxy PRRFC. The results show that the thermal and elastic properties depend on both constituent materials and the fiber volume ratio. The strength depends also on the type of applied stress. In general, no simple ratio exists between the properties of unidirectional fiber composites and those of PRRFC. The data are presented in convenient graphical form to serve as an aid for design and/or analysis and also for further research in PRRFC. The residual stresses and the impact resistance are also theoretically examined.
Document ID
19720010932
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1972
Subject Category
Materials, Nonmetallic
Report/Patent Number
E-6569
NASA-TN-D-6696
Report Number: E-6569
Report Number: NASA-TN-D-6696
Accession Number
72N18582
Funding Number(s)
PROJECT: RTOP 134-14
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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