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Multidisciplinary Design Of Hot Composite StructuresUnified computer code developed to implement multidisciplinary approach to design and analysis of composite-material structures that must withstand high temperatures. Code modular: includes executive module communicating with and coordinating other modules performing calculations pertaining to traditionally separate disciplines like those of acoustics, structural vibrations, structural loads, and thermal effects. Essential feature, finite-element numerical simulation of relevant physical phenomena according to applicable disciplines. Same finite-element mesh used in thermal, vibrational, and structural analyses; minimizing data-preparation time and eliminating errors incurred in transforming temperatures from one finite-element mesh to another.
Document ID
19960018787
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Chamis, Christos C.
(NASA Lewis Research Center, Cleveland, OH.)
Singhal, Surendra N.
(NYMA, Inc.)
Date Acquired
August 17, 2013
Publication Date
March 1, 1996
Publication Information
Publication: NASA Tech Briefs
ISSN: 0145-319X
Subject Category
Materials
Report/Patent Number
LEW-15977
Accession Number
96B10092
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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