The purpose of this study is to present a simplified semi-analytical method
ology to predict the behaviour of longitudinal cracks in cracked stiffened
curved panels with frames. Pressure loading acting on the longitudinal crac
ks induces geometrical non-linearity due to large deflections of crack edge
s. This methodology is based mainly on the application of "bulging" coeffic
ients to stress intensity factors taken from a numerical model of a stiffen
ed cracked flat panel in order to get the crack driving force of the curved
panel. This flat model must be geometrically similar to the curved panel.
The advantage of the method is the reduced calculation time compared with a
numerical model of the cracked stiffened curved panel, including frames. A
nalysis of the results shows a highly satisfactory correlation between pred
iction by calculation and experimental data. (C) 2001 Elsevier Science Ltd.
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