Characterization of Delaminations and Transverse Matrix Cracks in Composite Laminates Using Multiple-Angle Ultrasonic InspectionDelaminations and transverse matrix cracks often appear concurrently in composite laminates. Normal-incidence ultrasound is excellent at detecting delaminations, but is not optimum for matrix cracks. Non-normal incidence, or polar backscattering, has been shown to optimally detect matrix cracks oriented perpendicular to the ultrasonic plane of incidence. In this work, a series of six composite laminates containing slots were loaded in tension to achieve various levels of delamination and ply cracking. Ultrasonic backscattering was measured over a range of incident polar and azimuthal angles, in order to characterize the relative degree of damage of the two types. Sweptpolar- angle measurements were taken with a curved phased array, as a step toward an array-based approach to simultaneous measurement of combined flaws.
Document ID
20120016954
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Johnston, Patrick H. (NASA Langley Research Center Hampton, VA, United States)
Appleget, Chelsea D. (NASA Langley Research Center Hampton, VA, United States)
Odarczenko, Michael T. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
July 15, 2012
Subject Category
Composite Materials
Report/Patent Number
NF1676L-15216Report Number: NF1676L-15216
Meeting Information
Meeting: 39th Annual Review of Progress in Quantitative Nondestructive Evaluation (QNDE) Conference