The presence of dissimilar material systems and thermal gradients introduce
thermal stresses in multi-layered electronic assemblies and packages durin
g fabrication and operation. The high stress gradients near the free edge o
f bonding interfaces of such structures may cause cracking and delamination
leading to the failure or malfunction of electronic assemblies and package
s. A simple but accurate engineering approach for the calculation of interl
aminar thermal stresses due to thermal mismatch in multi-layered structures
is needed so that designers can determine interlaminar thermal stresses ea
sily without much computational efforts. A few approaches based on the gene
ralized deformation theory have been published but most of them are only su
itable for structures with symmetric layers. For electronic packages and as
semblies, unsymmetric layers are often used. An improved approach, Classica
l Laminate Theory-Edge Stress Shape (CLT-ESS), for prediction of interlamin
ar thermal stresses that can be applied to multi-layered structures with un
symmetric layers is presented. Comparisons are made with finite element ana
lysis results and are found to be favorable. The proposed approach provides
an efficient way for the calculation of interlaminar thermal stresses. [S1
043-7398(00)00901-4].