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Fundamental aspects of and failure modes in high-temperature composites
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ginty, Carol A. Chamis, Christos C. |
| Copyright Year | 1990 |
| Description | Fundamental aspects of and attendant failure mechanisms for high temperature composites are summarized. These include: (1) in-situ matrix behavior; (2) load transfer; (3) limits on matrix ductility to survive a given number of cyclic loadings; (4) fundamental parameters which govern thermal stresses; (5) vibration stresses; and (6) impact resistance. The resulting guidelines are presented in terms of simple equations which are suitable for the preliminary assessment of the merits of a particular high temperature composite in a specific application. |
| File Size | 629626 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19900010835 |
| Archival Resource Key | ark:/13960/t2b905g3b |
| Language | English |
| Publisher Date | 1990-01-01 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Ceramic Matrix Composites Vibration Temperature Effects Ductility Failure Analysis Failure Modes Impact Resistance Metal Matrix Composites High Temperature Thermal Stresses Loads Forces Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
