Once you solve a fracture application with StressCheck, you won’t want to use another FEA tool for that purpose again. You will experience ease of use, realize superconvergent extractions and receive the high definition feedback you need to guarantee the reliability and accuracy of the computed stress intensity factors (SIF) and energy release rates (ERR).
Fracture Mechanics Applications
StressCheck is ideally suited for damage tolerance and forensic engineers who need the best representation of 2D or 3D SIF’s, ERR’s and beta factors for input in sophisticated crack growth simulations, or when analyzing repairs for mitigation of cracks.
Schedule a Fracture Mechanics Demo
Would you like a no-cost demonstration of our fracture mechanics and DaDT engineering application solutions? Complete our Request an Engineering Application Demo form and we will get back to you shortly.
Fracture Mechanics Application Focus
The following are typical fracture mechanics analysis applications which are routinely performed in StressCheck Professional:
Linear Elasticity Solver
Fracture Mechanics Module
MeshSim Advanced Automesher
Linear Elasticity Solver
Fracture Mechanics Module
MeshSim Advanced Automesher
Linear Elasticity Solver
Fracture Mechanics Module
MeshSim Advanced Automesher
Would you like to schedule a Fracture Mechanics Analysis Demo?
Would you like to learn more about our features and solutions for fracture mechanics and DaDT analysis applications? Schedule a Fracture Mechanics Analysis demo with us by completing the below form and we’ll contact you as soon as possible. Thank you!
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Testimonials
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“A screening of existent commercial and non-commercial tools was carried out in respect to their fracture mechanics capabilities, their design abilities, implementation as well as their complexity. Although, there are many software possibilities, only those within the reach of the author were evaluated. This resulted in the selection of the commercial tool StressCheck. The assessment of crack propagation on compact tension and two stringer specimens governed by the Paris and Forman regimes was satisfactory compared with experimental results using the material data from simple standard specimens.”
Lloren Llopart Prieto (EADS)
Doctoral Thesis, "Modelling and analysis of crack turning on aeronautical structures"