A computer code, HITCAN (High Temperature Composite Analyzer) has been 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 structure level and 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.
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April 1992
Research Papers
HITCAN for Actively Cooled Hot-Composite Thermostructural Analysis
C. C. Chamis,
C. C. Chamis
NASA Lewis Research Center, Cleveland, OH 44135
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P. L. N. Murthy,
P. L. N. Murthy
NASA Lewis Research Center, Cleveland, OH 44135
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S. N. Singhal,
S. N. Singhal
Sverdrup Technology, Inc., Cleveland, OH 44142
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J. J. Lackney
J. J. Lackney
Sverdrup Technology, Inc., Cleveland, OH 44142
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C. C. Chamis
NASA Lewis Research Center, Cleveland, OH 44135
P. L. N. Murthy
NASA Lewis Research Center, Cleveland, OH 44135
S. N. Singhal
Sverdrup Technology, Inc., Cleveland, OH 44142
J. J. Lackney
Sverdrup Technology, Inc., Cleveland, OH 44142
J. Eng. Gas Turbines Power. Apr 1992, 114(2): 315-320 (6 pages)
Published Online: April 1, 1992
Article history
Received:
February 20, 1991
Online:
April 24, 2008
Citation
Chamis, C. C., Murthy, P. L. N., Singhal, S. N., and Lackney, J. J. (April 1, 1992). "HITCAN for Actively Cooled Hot-Composite Thermostructural Analysis." ASME. J. Eng. Gas Turbines Power. April 1992; 114(2): 315–320. https://doi.org/10.1115/1.2906589
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