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Second Generation Integrated Composite Analyzer (ICAN) Computer CodeThis manual updates the original 1986 NASA TP-2515, Integrated Composite Analyzer (ICAN) Users and Programmers Manual. The various enhancements and newly added features are described to enable the user to prepare the appropriate input data to run this updated version of the ICAN code. For reference, the micromechanics equations are provided in an appendix and should be compared to those in the original manual for modifications. A complete output for a sample case is also provided in a separate appendix. The input to the code includes constituent material properties, factors reflecting the fabrication process, and laminate configuration. The code performs micromechanics, macromechanics, and laminate analyses, including the hygrothermal response of polymer-matrix-based fiber composites. The output includes the various ply and composite properties, the composite structural response, and the composite stress analysis results with details on failure. The code is written in FORTRAN 77 and can be used efficiently as a self-contained package (or as a module) in complex structural analysis programs. The input-output format has changed considerably from the original version of ICAN and is described extensively through the use of a sample problem.
Document ID
19930008950
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Murthy, Pappu L. N.
(NASA Lewis Research Center Cleveland, OH, United States)
Ginty, Carol A.
(NASA Lewis Research Center Cleveland, OH, United States)
Sanfeliz, Jose G.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Subject Category
Composite Materials
Report/Patent Number
E-6831
Report Number: E-6831
Accession Number
93N18139
Funding Number(s)
PROJECT: RTOP 505-63-5B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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