Loading...
Please wait, while we are loading the content...
Similar Documents
High temperature composite analyzer (hitcan) user's manual, version 1.0
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Gotsis, P. Singhal, S. N. Murthy, P. L. N. Lackney, J. J. |
| Copyright Year | 1993 |
| Description | This manual describes 'how-to-use' the computer code, HITCAN (HIgh Temperature Composite ANalyzer). HITCAN is a general purpose computer program for predicting nonlinear global structural and local stress-strain response of arbitrarily oriented, multilayered high temperature metal matrix composite structures. This code combines composite mechanics and laminate theory with an internal data base for material properties of the constituents (matrix, fiber and interphase). The thermo-mechanical properties of the constituents are considered to be nonlinearly dependent on several parameters including temperature, stress and stress rate. The computation procedure for the analysis of the composite structures uses the finite element method. HITCAN is written in FORTRAN 77 computer language and at present has been configured and executed on the NASA Lewis Research Center CRAY XMP and YMP computers. This manual describes HlTCAN's capabilities and limitations followed by input/execution/output descriptions and example problems. The input is described in detail including (1) geometry modeling, (2) types of finite elements, (3) types of analysis, (4) material data, (5) types of loading, (6) boundary conditions, (7) output control, (8) program options, and (9) data bank. |
| File Size | 5510477 |
| Page Count | 182 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930015881 |
| Archival Resource Key | ark:/13960/t9n34s38f |
| Language | English |
| Publisher Date | 1993-04-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Fiber Composites Mechanical Properties Boundary Conditions Laminates User Manuals Computer Programs Computer Programs Fortran Finite Element Method Micromechanics Stress-strain Relationships Fiber-matrix Interfaces Metal Matrix Composites Composite Structures Buckling Structural Analysis Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |