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ICAN: Integrated composites analyzerThe ICAN computer program performs all the essential aspects of mechanics/analysis/design of multilayered fiber composites. Modular, open-ended and user friendly, the program can handle a variety of composite systems having one type of fiber and one matrix as constituents as well as intraply and interply hybrid composite systems. It can also simulate isotropic layers by considering a primary composite system with negligible fiber volume content. This feature is specifically useful in modeling thin interply matrix layers. Hygrothermal conditions and various combinations of in-plane and bending loads can also be considered. Usage of this code is illustrated with a sample input and the generated output. Some key features of output are stress concentration factors around a circular hole, locations of probable delamination, a summary of the laminate failure stress analysis, free edge stresses, microstresses and ply stress/strain influence coefficients. These features make ICAN a powerful, cost-effective tool to analyze/design fiber composite structures and components.
Document ID
19840018687
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Murthy, P. L. N.
(NASA Lewis Research Center Cleveland, OH, United States)
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-83700
E-2158
NAS 1.15:83700
Report Number: NASA-TM-83700
Report Number: E-2158
Report Number: NAS 1.15:83700
Meeting Information
Meeting: Struct., Struct. Dyn. and Mater. Conf.
Location: Palm Springs, CA
Country: United States
Start Date: May 14, 1984
End Date: May 16, 1984
Sponsors: ASME, AHS, ASCE, AIAA
Accession Number
84N26755
Funding Number(s)
PROJECT: RTOP 505-33-58
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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