The classical Savin solution for the stress induced in an orthotropic plate
containing an ellipitical hole places no restrictions on remote rigid-body
rotations. In this paper the Savin procedure is used to obtain a solution
for which remote rigid-body rotations are required to be zero. The validity
of these new results is demonstrated by comparing predicted displacement f
ields near a circular hole in specially orthotropic composite panels with t
hose measured using moire techniques as well as those predicted using the f
inite element method.