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“In the case of the through crack configuration, the comparison of experimental and StressCheck derived geometry factors showed a close correlation and were an improvement to solutions provided in AFGROW at the time. Based on the results of this research, StressCheck pin-loaded lug geometry factors have since been incorporated into the AFGROW software.”

Dr. Alten Grandt, Purdue University

The ESRD Resource Library

The ESRD Resource Library

Computation of SIFs in StressCheck

Crack Path Analysis Technical Brief

Deployment of Smart Simulation Apps in Support of DaDT Activities

Equilibrium of nodal forces in the h- and p-versions of the FEM

Fatigue Life Prediction of Flaw-Tolerant Damaged Rotorcraft Structures

Helpful Hints and Tips: Converting from Shear to Normal Stress-Strain Diagram

Helpful Hints and Tips: Elliptical Crack Automeshing Guidelines

History and Use of High Order Finite Element Methods in Professional Practice

Incremental Plasticity Hardening Models – An Introduction

Incremental Plasticity Technical Brief

Integrating Residual Stress Analysis of Critical Fastener Holes into USAF Depot Maintenance

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The ESRD Resource Library

Computation of SIFs in StressCheck

Crack Path Analysis Technical Brief

Deployment of Smart Simulation Apps in Support of DaDT Activities

Eigenvalue convergence in the p-version of the FEM

Equilibrium of nodal forces in the h- and p-versions of the FEM

Fatigue Life Prediction of Flaw-Tolerant Damaged Rotorcraft Structures

Helpful Hints and Tips: Converting from Shear to Normal Stress-Strain Diagram

Helpful Hints and Tips: Elliptical Crack Automeshing Guidelines

History and Use of High Order Finite Element Methods in Professional Practice

Incremental Plasticity Hardening Models – An Introduction

Incremental Plasticity Technical Brief

Integrating Residual Stress Analysis of Critical Fastener Holes into USAF Depot Maintenance

Search Resources