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ASTM E2580-17

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ASTM E2580-17

Standard Practice for Ultrasonic Testing of Flat Panel Composites and Sandwich Core Materials Used in Aerospace Applications

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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
Set ASTMVOL0304
Year 2017
Document history ASTM E2580-12
Country USA
Keyword ASTM 2580;ASTM E2580;ASTM E2580;10.1520/E2580-17