An analysis method suitable for prediction of strain fields in a stiff
ened composite panel containing a center crack is presented. The analy
sis is based on the superposition of anisotropic elasticity solutions
for an infinite plate. Strain field predictions are made for two panel
configurations and compared with strain gage data. Reasonable compari
sons between predictions and measurements are obtained. This paper lay
s the foundation for the predictions of the damage tolerance of stiffe
ned composite panels that will be discussed further in a second paper.