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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“Through the use of StressCheck the A-10 Aircraft Structural Integrity Program’s (ASIP) Analysis Group is able to model more accurately the physics of fatigue crack propagation in critical aircraft structure. Through this tool we are able to model, analyze and predict failure of aircraft structure and then develop crucial inspection and maintenance planes to ensure the safety and sustainability of our nations warplanes. Without the analysis capability provided to us through StressCheck we would not be able to provide accurate assessments of the A-10 structure to top USAF leadership.”
SWRI Research Engineer
Southwest Research Institute