Analytical solutions are sought for optimal temperature distributions to control interlaminar stresses near the free edges of composite laminates subjected to uniaxial loading. Thermal gradients are obtained by minimizing appropriate performance indices that are functions of the far field properties with respect to the through thickness temperature differences. It is shown that a uniform temperature drop or rise can completely eliminate all of the interlaminar stresses for cross or angle ply laminates and for other laminates, nonuniform temperature distributions must be applied to minimize the stresses.
|Number of pages||11|
|Journal||Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference|
|State||Published - 1994|
|Event||Proceedings of the 35th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Part 1 (of 5) - Hilton Head, SC, USA|
Duration: Apr 18 1994 → Apr 20 1994