StressCheck Tutorial: Solution Process Monitoring (CPU, RAM, Disk I/O Usage)
Abstract: benchmark of 9532 3D elements (9160 tetrahedra, 212 pentahedra and 160 hexahedra) of a longeron section under bearing/bypass loading was solved at p=6 (~1.1M DOF, 7 minutes) in StressCheck v11 Update 1 and required 17 GB of disk space and approximately 3.3 GB of RAM during solution processing.
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“As the United States Air Force continues to extend the service life of their aircraft the Aircraft Structural Integrity Program (ASIP) has had to refine the methods it uses to analyze and predict fatigue crack growth. Through the use StressCheck®, coupled with AFGROW, we in A-10 ASIP have been able to more accurately model, predict and analyze critical aircraft structure for the A-10 and other types of structure for non-A-10 system managers. This also allows us within the A-10 to more accurately assess risk for decision makers, streamline aircraft inductions into scheduled maintenance and reduce cost for total life cycle management.”
A-10 ASIP Manager