Helpful Hints and Tips: Application of TLAP Bearing to HyperMesh Import
Abstract: Importing a HyperMesh solver deck (.NAS) of 2nd order tetra elements and assigning a point load to a geometry-less hole via TLAP-Bearing application.
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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