Fatigue Module

Software for Stress- and Strain-Based, High- and Low-Cycle Fatigue Analysis

Fatigue Module

Low-cycle fatigue resulting from plastic deformation near a hole showing the logarithm of lifetime in terms of number of cycles together with a stress-strain curve for the first few load cycles.

Fatigue Analysis for Many Different Structures and Applications

When structures are subjected to repeated loading and unloading due to material fatigue, they can fail at loads below the static limit. A virtual fatigue analysis can be performed in the COMSOL Multiphysics environment with the Fatigue Module, an add-on to the Structural Mechanics Module. With the stress-based and the strain-based critical plane methods, you can evaluate the high-cycle and low-cycle fatigue regime. In applications involving nonlinear materials you can use energy-based methods or Coffin-Manson type models to simulate thermal fatigue.

When dealing with variable loads, the accumulated damage can be calculated from the load history and the fatigue limit. The fatigue load cycle can be simulated in solid bodies, plates, shells, multibodies, applications involving thermal stress and deformation, and even on piezoelectric devices. In order to improve computational efficiency when dealing with subsurface or surface initiated fatigue, a fatigue evaluation can be performed on domains, boundaries, lines and in points.

Stress- and Strain-Based Critical Plane Models

Critical plane models search for a plane that is most favorable for crack initiation and propagation where fatigue will take place. These are available in the Fatigue Module for both the stress- and strain-based models. In the high-cycle fatigue domain, where plasticity is very limited, stress-based models are typically used. In the Fatigue Module, they are calculated through the Findley, Normal stress, and Matake criteria, which calculate the fatigue usage factor that is compared to the fatigue limit.

Strain-based models evaluate strains or combinations of strains and stresses when defining a critical plane. Once the critical plane is identified, they predict the number of cycles to failure. The Fatigue Module features the Smith-Watson-Topper (SWT), Fatemi-Socie, and Wang-Brown models. These models are usually used in low-cycle fatigue where the strains are large. The Neuber's rule and the Hoffmann-Seeger method are available to approximate the effect of plasticity in a quick linear-elastic simulation. It is also possible to consider a full elastoplastic fatigue cycle when using the Nonlinear Structural Materials Module.

Fatigue Analysis of a Wheel Rim

High-Cycle Fatigue Analysis of a Cylindrical Test Specimen

Thermal Fatigue of a Surface Mount Resistor

Fatigue Response of a Random Non-Proportional Load

Cycle Counting in Fatigue Analysis - Benchmark

Submodeling of Thermal Fatigue in a Ball Grid Array

Notch Approximation to Low-Cycle Fatigue Analysis of Cylinder with a Hole

Elastoplastic Low-Cycle Fatigue Analysis of Cylinder with a Hole

Fatigue Analysis of a Non-Proportionally Loaded Shaft with a Fillet