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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: TLAP-Traction vs Uniform Traction Case Study

StressCheck Tutorial: Toolbars and Selectors Overview

StressCheck Tutorial: Torque Bar Analysis

StressCheck Tutorial: Traction Load

StressCheck Tutorial: Transitioning from Part Thru to Thru Crack

StressCheck Tutorial: Tube Creation by Sweep Method

StressCheck Tutorial: Usage of the Force/Moment Method for Arbitrary Cross Sections

StressCheck Tutorial: Using Cutting Planes for Model Viewing and Live Results Processing

StressCheck Tutorial: Using Edit Toolbar for Object Selection and Visualization

StressCheck Tutorial: Using Max Stress Location for New Extractions

StressCheck Tutorial: Using Sets

StressCheck Tutorial: Using the Set Method for Results Processing

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