ABSTRACT--This paper suggests a very simple, force-based formula that combines four failure modes into one dimensionless equation to govern spot weld failure under general static loading conditions. The four failure modes are shear, rotation, normal and peel. The normal separation mode and the peel mode are corresponding to mode I (opening mode). The tensile/shear mode is mode II (sliding mode), and the in-plane rotation mode is mode III (tearing mode). Test coupons and test fixtures are designed and tested to establish and verify this equation. To further verify this equation, a long difficult to understand automotive spot weld failure problem was studied. Applying finite element-calculated resultant loads to the proposed formula resulted in analytical values that correlated very well with the long time field observed spot weld failures. This analytical prediction reasonably explained the spot weld failure mechanism and provided good design directions to improve the durability of the auto structure.KEY WORDS--Spot weld, complete failure modes, forcebased failure criterion, semi-empirical method, test coupon for verificationTo understand and accurately predict spot weld failure is very important in auto body shell structure design. Numerous efforts have been devoted to estimating the fatigue life of spot welds.I-4 Few stress-based multiaxial failure criteria 5-7 have been published for spot weld fatigue failure prediction. These criteria, in general, are based on high-cycle/low-stress fatigue tests for the overlap shear mode and peel mode only. Spot weld failure criteria for the low-cycle/high-stress, normal separation mode and in-plane rotation modes are extremely rare. Spot weld designs using these criteria with simplified finite element modeling earl lead to (1) underestimated stresses by rigid bar simulation, (2) lack of data support for high-stress/low-cycle failure, and (3) incomplete failure mode consideration. Due to geometric complexity and material nonhomogeneity, it is impractical to accurately model each spot weld using detailed solid elements, since about 5000 to 11000 quadratic solid elements are required. Currently, in the automotive industry, the most common method of modeling a spot weld is to use rigid-bar links. A spot weld, in spite of the fact that it is not a slender structure, is modeled as a rigid bar. By definition, the dependent node of a rigid bar would follow the independent node in the specified degree of freedom that artificially constrains the local deformation of the rigid bar in the coupled degree of freedom. Apparently, Engineer, MD44 AEC Building, Ford Motor Company, Dearborn, MI 48121. Original manuscript submitted." August 16, 2000. Final manuscript received: November 1, 2000 this modeling technique cannot provide correct strains and stresses in the vicinity of the spot weld. On the other hand, due to cost-saving considerations, auto industries do require simple finite element model representation of spot welds.
P. Wung is a ResearchIn addition to the finite element modeli...