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User's Manual and Final Report for Hot-SMAC GUI DevelopmentA new software package called Higher Order Theory-Structural/Micro Analysis Code (HOT-SMAC) has been developed as an effective alternative to the finite element approach for Functionally Graded Material (FGM) modeling. HOT-SMAC is a self-contained package including pre- and post-processing through an intuitive graphical user interface, along with the well-established Higher Order Theory for Functionally Graded Materials (HOTFGM) thermomechanical analysis engine. This document represents a Getting Started/User's Manual for HOT-SMAC and a final report for its development. First, the features of the software are presented in a simple step-by-step example where a HOT-SMAC model representing a functionally graded material is created, mechanical and thermal boundary conditions are applied, the model is analyzed and results are reviewed. In a second step-by-step example, a HOT-SMAC model of an actively cooled metallic channel with ceramic thermal barrier coating is built and analyzed. HOT-SMAC results from this model are compared to recently published results (NASA/TM-2001-210702) for two grid densities. Finally, a prototype integration of HOTSMAC with the commercially available HyperSizer(R) structural analysis and sizing software is presented. In this integration, local strain results from HyperSizer's structural analysis are fed to a detailed HOT-SMAC model of the flange-to-facesheet bond region of a stiffened panel. HOT-SMAC is then used to determine the peak shear and peel (normal) stresses between the facesheet and bonded flange of the panel and determine the "free edge" effects.
Document ID
20020011362
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Yarrington, Phil
(Collier Research and Development Corp. Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
November 1, 2001
Subject Category
Computer Programming And Software
Report/Patent Number
NASA/CR-2001-211294
NAS 1.26:211294
E-13088
Report Number: NASA/CR-2001-211294
Report Number: NAS 1.26:211294
Report Number: E-13088
Funding Number(s)
CONTRACT_GRANT: NAS3-00159
PROJECT: RTOP 251-30-07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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