Abstract: A method for identifying types of flaws in a composite object includes: a) rapidly heating the surface of the object; b) recording pixel intensities in a sequence of IR images; c) determining temperature-versus-time data for each of the pixels from the IR images; and d) determining what type of flaw if any corresponds to each of the pixels using the temperature-versus-time data determined in step (c). A contrast curve derived from the temperature-versus-time data may be used in determining what type of flaws if any corresponds to each of the pixels. The contrast curve may be determined by subtracting a synthetic reference curve from a temperature time curve from the temperature-versus-time data. The types of flaws may be determined from size and/or shapes of peaks in the contrast curves. Some flaws are delaminations, layers of porosity, and uniformly distributed porosity.

Abstract: A method and system for determining thermal diffusivity and porosity of an article are provided. The method comprises heating a surface of the article, capturing image data corresponding to an evolution of lateral heat flow from the surface of the article, applying a thermal time of flight analysis on the image data and determining thermal diffusivity and porosity values of the article using the thermal time of flight analysis for the lateral heat flow.

Abstract: A system for locating a failure event in a sample is disclosed. The system includes at least one sensor configured to detect acoustic energy corresponding to the failure event in the sample. The system also includes an infrared camera configured to detect a thermal release of energy corresponding to the failure event in the sample.

Abstract: A method and system for determining thermal diffusivity and porosity of an article are provided. The method comprises heating a surface of the article, capturing image data corresponding to an evolution of lateral heat flow from the surface of the article, applying a thermal time of flight analysis on the image data and determining thermal diffusivity and porosity values of the article using the thermal time of flight analysis for the lateral heat flow.

Abstract: A non-destructive evaluation system and method is provided for detecting flaws in an object. The system includes a lamp for impinging the object with optical pulses and a focal plane array camera configured to capture the images corresponding to evolution of heat due to an impact of the optical pulses in the object. The system also includes an image acquisition system for capturing data corresponding to the images from the focal plane array camera. Both transmission mode imaging and reflection mode imaging techniques are used in an exemplary embodiment. A time of flight analysis system is also provided for analyzing the data from both transmission mode imaging technique and reflection mode imaging technique. The data from transmission mode imaging is used to determine thickness values at different points in the data and for determining location of flaws using the thickness values. The data from reflection mode imaging is used for determining depth of these flaws.

Abstract: A system for locating a failure event in a sample is disclosed. The system includes at least one sensor configured to detect acoustic energy corresponding to the failure event in the sample. The system also includes an infrared camera configured to detect a thermal release of energy corresponding to the failure event in the sample.