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1.1 This practice establishes two procedures for ultrasonic testing (UT) of flat panel composites and flat sandwich core panels (parallel surfaces). Typical as-fabricated lay-ups include uniaxial, cross ply and angle ply laminates; as well as honeycomb sandwich core materials. These procedures can be used throughout the life cycle of the materials; product and process design optimization, on line process control, after manufacture inspection, and in service inspection. Contact methods such as angle-beam techniques using shear waves, or surface-beam techniques using Lamb waves, are not discussed.
| Author | ASTM |
|---|---|
| Editor | ASTM |
| Document type | Standard |
| Format | File |
| ICS | 49.035 : Components for aerospace construction |
| Number of pages | 7 |
| Replace | ASTM E2580-12 + Redline |
| Set | ASTMVOL0304 |
| Year | 2017 |
| Document history | ASTM E2580-12 + Redline |
| Country | USA |
| Keyword | ASTM 2580;ASTM E2580;ASTM E2580;10.1520/E2580-17 |