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Demonstration of capabilities of high temperature composites analyzer code HITCANThe capabilities a high temperature composites analyzer code, HITCAN which predicts global structural and local stress-strain response of multilayered metal matrix composite structures, are demonstrated. The response can be determined both at the constituent (fiber, matrix, and interphase) and the structure level and includes the fabrication process effects. The thermo-mechanical properties of the constituents are considered to be nonlinearly dependent on several parameters including temperature, stress, and stress rate. The computational procedure employs an incremental iterative nonlinear approach utilizing a multifactor-interactive constituent material behavior model. Various features of the code are demonstrated through example problems for typical structures.
Document ID
19900010313
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Singhal, Surendra N.
(Sverdrup Technology, Inc., Cleveland OH., United States)
Lackney, Joseph J.
(Sverdrup Technology, Inc., Cleveland OH., United States)
Chamis, Christos C.
(NASA Lewis Research Center Cleveland, OH., United States)
Murthy, Pappu L. N.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1990
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-102560
E-5380
NAS 1.15:102560
Report Number: NASA-TM-102560
Report Number: E-5380
Report Number: NAS 1.15:102560
Accession Number
90N19629
Funding Number(s)
PROJECT: RTOP 763-01-4B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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