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ASTM E2582-19

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Standard Practice for Infrared Flash Thermography of Composite Panels and Repair Patches Used in Aerospace Applications

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1.1 This practice describes a procedure for detecting subsurface flaws in composite panels and repair patches using Flash Thermography (FT), in which an infrared (IR) camera is used to detect anomalous cooling behavior of a sample surface after it has been heated with a spatially uniform light pulse from a flash lamp array.

Author ASTM
Editor ASTM
Document type Standard
Format File
ICS 49.035 : Components for aerospace construction
Number of pages 6
Replace ASTM E2582-07(2014)
Year 2019
Document history ASTM E2582-07(2014)
ASTM E2582-07
Country USA
Keyword ASTM 2582;ASTM E2582;ASTM E2582;10.1520/E2582-19