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1.1 This test method covers the in-plane compressive properties of polymer matrix composite materials reinforced by high-modulus fibers in a sandwich beam configuration. The composite material forms are limited to continuous-fiber composites of unidirectional orientation. This test procedure introduces compressive load into a thin skin bonded to a thick honeycomb core with the compressive load transmitted into the sample by subjecting the beam to four-point bending.
| Author | ASTM |
|---|---|
| Editor | ASTM |
| Document type | Standard |
| Format | File |
| Confirmation date | 2017-01-01 |
| ICS | 83.120 : Reinforced plastics |
| Number of pages | 10 |
| Replace | ASTM D5467/D5467M-97(2010) |
| Set | ASTMVOL1503 |
| Year | 1990 |
| Document history | ASTM D5467/D5467M-97(2010) |
| Country | USA |
| Keyword | ASTM 5467;ASTM D5467;ASTM D5467;10.1520/D5467_D5467M-97R17 |