NASA NTRS · 20080004863
Method and apparatus for thermographically and quantitatively analyzing a structure for disbonds and/or inclusions
Abstract
A heat source such as a magnetic induction/eddy current generator remotely heats a region of a surface of a test structure to a desired depth. For example, the frequency of the heating source can be varied to heat to the desired depth. A thermal sensor senses temperature changes in the heated region as a function of time. A computer compares these sensed temperature changes with calibration standards of a similar sample having known disbond and/or inclusion geography(ies) to analyze the test structure. A plurality of sensors can be arranged linearly to sense vector heat flow.
Keep this discovery
Explore connections, maps & timelines
Heyman, Joseph S., Winfree, William P., Cramer, K. Elliott, Zalamedia, Joseph N.. 1996-10-08. Method and apparatus for thermographically and quantitatively analyzing a structure for disbonds and/or inclusions. https://ntrs.nasa.gov/citations/20080004863
Cite the original work for its findings. Save a collection to share your selection of sources.