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Lamb Wave Tomography for Corrosion MappingAs the world-wide civil aviation fleet continues to age, methods for accurately predicting the presence of structural flaws-such as hidden corrosion-that compromise airworthiness become increasingly necessary. Ultrasonic guided waves, Lamb waves, allow large sections of aircraft structures to be rapidly inspected. However, extracting quantitative information from Lamb wave data has always involved highly trained personnel with a detailed knowledge of mechanical-waveguide physics. Our work focuses on using a variety of different tomographic reconstruction techniques to graphically represent the Lamb wave data in images that can be easily interpreted by technicians. Because the velocity of Lamb waves depends on thickness, we can convert the travel times of the fundamental Lamb modes into a thickness map of the inspection region. In this paper we show results for the identification of single or multiple back-surface corrosion areas in typical aluminum aircraft skin structures.
Document ID
19990028753
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Hinders, Mark K.
(College of William and Mary Williamsburg, VA United States)
McKeon, James C. P.
(College of William and Mary Williamsburg, VA United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 1999
Publication Information
Publication: The Second Joint NASA/FAA/DoD Conference on Aging Aircraft
Issue: Pt. 2
Subject Category
Structural Mechanics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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