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Optimal Synthesis of Hot Composite Laminates with Interphase LayersA method for the optimal grading of a single interphase layer in metal matrix composite laminates for the minimization of residual stresses is described. The capability to simultaneously tailor some fabrication parameters is also incorporated. Applications for unidirectional, cross-ply and quasi-isotropic Graphite/Copper laminates are investigated to assess the potential of interphase layer in reducing matrix residual stresses in various laminate configurations. Simultaneous optimization of interphase and fabrication characteristics appears to be more effective in decreasing residual stresses. The results also indicate that the interphase layer is more effective in lowering residual stresses in unidirectional composites and selectively within individual plies of a laminate. Embedded interphase layers in all the plies did not produce a significant global reduction in residual stresses.
Document ID
19940009569
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rabzak, Christopher
(Sverdrup Technology, Inc. Brook Park, OH., United States)
Saravanos, Dimitris A.
(NASA Lewis Research Center Cleveland, OH, United States)
Chamis, Christos C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1993
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-106326
NAS 1.15:106326
E-8081
Report Number: NASA-TM-106326
Report Number: NAS 1.15:106326
Report Number: E-8081
Meeting Information
Meeting: Symposium on Functionally Graded, Advanced Composite Materials
Location: Charlottesville, VA
Country: United States
Start Date: June 6, 1993
End Date: June 9, 1993
Sponsors: SES, ASCE, ASME
Accession Number
94N14042
Funding Number(s)
PROJECT: RTOP 510-01-50
Distribution Limits
Public
Copyright
Public Use Permitted.
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