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HITCAN for actively cooled hot-composite thermostructural analysisA computer code, high temperature composite analyzer (HITCAN), was developed to analyze/design hot metal matrix composite structures. HITCAN is a general purpose code for predicting the global structural and local stress-strain response of multilayered (arbitrarily oriented) metal matrix structures both at the constituent (fiber, matrix, and interphase) and the structural level, including the fabrication process effects. The thermomechanical 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-interaction material behavior model, i.e., the material properties are expressed in terms of a product of several factors that affect the properties. HITCAN structural analysis capabilities (static, load stepping - a multistep static analysis with material properties updated at each step, modal, and buckling) for cooled hot structures are demonstrated through a specific example problem.
Document ID
19920054272
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Murthy, P. L. N.
(NASA Lewis Research Center Cleveland, OH, United States)
Singhal, S. N.
(NASA Lewis Research Center Cleveland, OH, United States)
Lackney, J. J.
(Sverdrup Technology, Inc. Cleveland, OH, United States)
Date Acquired
August 15, 2013
Publication Date
April 1, 1992
Publication Information
Publication: ASME, Transactions, Journal of Engineering for Gas Turbines and Power
Volume: 114
Issue: 2 Ap
ISSN: 0742-4795
Subject Category
Structural Mechanics
Report/Patent Number
ASME PAPER 91-GT-116
Accession Number
92A36896
Distribution Limits
Public
Copyright
Other

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