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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

The ESRD Resource Library

The ESRD Resource Library

StressCheck Tutorial: Extracting Cut Section Stresses

StressCheck Tutorial: Extracting SIF Distributions Over Crack Front Segments

StressCheck Tutorial: Extraction a 2D Surface Profile from a 3D Solid

StressCheck Tutorial: Face to Face Meshing for TLAP Traction

StressCheck Tutorial: Fastener Element and General Nonlinear Analysis

StressCheck Tutorial: Feature-Based Mesh Refinement

StressCheck Tutorial: Filled vs Open Hole SIF Comparison for 3D Offset Hole

StressCheck Tutorial: Fitting + I-Beam Multi-Body Contact Analysis

StressCheck Tutorial: Force/Moment Load

StressCheck Tutorial: Getting Started with Excel VBA

StressCheck Tutorial: Getting Started with Python

StressCheck Tutorial: Global-Local with Multi-Body Contact

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