“…Delamination is supposed to start propagating when the sum 1521-3331/99$10.00 © 1999 IEEE of the stresses reaches a critical stress. On the other hand, sum of the stresses reaches the critical stress with a smaller load, because the shear stress due to bending acts in the direction which increases the residual stress Therefore, the true adhesion strength (critical shear stress) can be estimated by arithmetically averaging the apparent strength (shear stresses) due to bending alone, and These stress fields near the precrack tip caused by the critical bending loads and are expressed in terms of the stress intensity factor of the interface crack [8], [10] as and These apparent stress intensity factors can be calculated by a finite element method or by beam theory [6]. We can obtain the "true" adhesion strength which is not affected by residual stress, by calculating the average of and Adhesion strength was measured using two kinds of epoxy molding compounds and two kinds of lead frame materials (alloy 42 and copper) .…”