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Physical aging in graphite epoxy composites
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kong, E. S. W. |
| Copyright Year | 1981 |
| Description | The matrix dominated mechanical behavior of a graphite epoxy composite was found to be affected by sub Tg annealing. Postcured + or - 45 deg 4S specimens of Thornel 300 graphite/Narmco 5208 epoxy were quenched from above Tg and given a sub Tg annealing at 140 C for times up to 10 to the 5th power min. The ultimate tensile strength, strain to break, and toughness of the composite material were found to decrease as functions of sub Tg annealing time. No weight loss was observed during the sub Tg annealing. The time dependent change in mechanical behavior is explained on the basis of free volume changes that are related to the physical aging of the nonequilibrium glassy network epoxy. The results imply possible changes in composite properties with service time. |
| File Size | 869593 |
| Page Count | 26 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810012605 |
| Archival Resource Key | ark:/13960/t0zp8vb07 |
| Language | English |
| Publisher Date | 1981-04-01 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Quenching Cooling Prepregs Time Dependence Annealing Carbon Fibers Transition Temperature Aging Materials Mechanical Properties Graphite-epoxy Composites Amorphous Materials Matrix Materials 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 |