Conference Presentation: ASIP T-38 Vertical Tail Teardown Analysis

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Conference Presentation: ASIP T-38 Vertical Tail Teardown Analysis

Abstract: For the ASIP 2011 Conference, Northrop Grumman analysts presented a StressCheck modeling approach for generating custom beta factors to support T-38 vertical tail teardown analysis.

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Categories: Fracture Mechanics Module, Linear Elasticity Solver, MeshSim Advanced Module, StressCheck Core, StressCheck Professional. Tags: Damage Tolerance, Detailed Stress, Fracture Mechanics, Global-Local.

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“We have been having very good success using the P-Version finite element code, StressCheck^®, to develop the 2-D solutions for two independent cracks in a plate. I have asked one of our AFGROW team members to model the plate and lug cases using StressCheck^® and compare them to the existing AFGROW closed-form solutions. [He] modeled the cases several different ways to be sure that he was getting the best possible solutions. He has verified that the bearing load option in StressCheck^® provides excellent results.”
Jim Harter
Team Leader-Analytical Fatigue/Fracture Reliability Team Air Force Research Laboratory (AFRL)

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Conference Presentation: ASIP T-38 Vertical Tail Teardown Analysis