Non-destructive flaw sizing is an important part of the quality contro
l of materials. In composites, problems such as delaminations can cons
iderably reduce the effectiveness of such materials. Ultrasound is an
effective method for inspection of composites. However, owing to the h
igh degree of anisotropy in composites, ultrasonic inspection may prod
uce false or distorted information about the delamination. In this stu
dy, an iterative sizing technique has been developed that utilizes the
Gauss-Hermite beam model and Auld's reciprocity relation. The beam mo
del compensates for excessive beam spread in certain directions in com
posites. In this sizing method, a line scan of a circular delamination
is first obtained using the pulse-echo technique, and the resulting a
mplitude versus position data for a chosen frequency are fed to a comp
uter program. The computer program computes the size for a delaminatio
n that best fits the line scan result of the experiment. The sizing te
chnique was tested on a simulated delamination inside a unidirectional
graphite/epoxy composite. The results showed significant improvement
in sizing over the apparent size measurement based on the full width a
t the half maximum amplitude of the experimental line scan.