Meshing Archives

“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

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ASIP 2021 Training – Standardization and Automation of DaDT Solutions via FEA-Based Sim Apps

ASIP 2022 Training – Best Practices for the Modeling and Analysis of Bonded Doubler Repairs

ASIP 2023 Training – Enhancements in StressCheck v12.0 for DaDT Analysis of 3D Fastened Connections

ASIP 2024 Training – Case Studies in Fracture Mechanics Analysis Using StressCheck v12.0

Automatic Lamination: Countersink Bore

Computation of SIFs in StressCheck

DTA of Bonded Repairs on the Wing Skin of the C130 Using Finite Elements

Experimental Validation of DTA Modeling of Bonded Wing Skin Repairs

Getting Started with StressCheck: e-Learning Video Showcase

Helpful Hints and Tips: 3D Contact Analysis with Knuckle Joint

Helpful Hints and Tips: 3D Stiffened Lug Stress + Crack SIF Analyses

Helpful Hints and Tips: Adding Contact to a Hand Meshed Model

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