This paper presents a method of pinpointing structural damage locations usi
ng operational deflection shapes (ODSs) measured by a scanning laser vibrom
eter. The method assumes the form C-1 cos beta x + C-2 sin beta x + C-3 cos
h beta x + C-4 sinh beta x for an ODS to match with its experimental data u
sing a sliding-window least-squares method to determine the four coefficien
ts C-i. It is shown that C-1 represents the central solution of displacemen
t, C-3 the boundary-layer solution of displacement caused by boundary const
raints, C(2)beta the central solution of slope, and C(4)beta the boundary-l
ayer solution of slope. Moreover, C-1 * C-3 is Proportional to the differen
ce of kinetic and elastic energy densities, C-3 - C-1 is proportional to th
e curvature, and C-4 - C-2 is proportional to the spatial derivative of the
curvature. Because cracks on a structure introduce new boundaries to the s
tructure and these coefficients change significantly at boundaries, crack l
ocations are clearly revealed by the peaks on the C-1 * C-3 curve, Sign cha
nge of C-4, peaks on the fitting error curve, and sudden changes of C-3 - C
-1 and C-4 - C-2. Moreover, numerical and experimental results show that ea
ch of these coefficients requires a different length of data points for cur
ve fitting in order to smooth the curve. Based on this different data lengt
h requirement and the peaks and sign change of these coefficients we derive
a boundary effect detection (BED) method for finding damage locations. A n
on-linear sliding-window least-squares fitting technique is also derived fo
r estimating the extent of structural damage. Numerical and experimental st
udies on beams with different damages have been performed to prove the accu
racy and reliability of the BED method. (C) 2000 Academic Press.