Strategies for the automation of durability and damage tolerance (DaDT) solutions, driven by Sim Apps designed for the computation of FEA-based total beta factors, will be explored.
October 8, 2020 @ 1:00 pm EST
Introduction to Fracture Mechanics for DaDT Solution Automation
This webinar is now available to watch on-demand.
WEBINAR SUMMARY
In this pre-recorded 2 hour webinar we will discuss the creation of Sim Apps for the automatic generation of complex, solution-verified 2D and 3D beta factors via the integration of StressCheck's parametric FEA engine, the Windows Component Object Model (COM) and Microsoft Excel VBA.
WEBINAR HIGHLIGHTS
In Part 1 of this webinar series, the following topics are presented:
- 3D StressCheck Fracture Mechanics demo
- Overview of linear elastic fracture mechanics (LEFM) parameters for fatigue crack growth: SIF’s, J-integrals and beta factors.
- Computation of LEFM parameters in StressCheck.
- Beta factor compounding pros and cons.
- FEA-based total beta factors.
- Why use StressCheck for LEFM?
In Part 2 of this webinar series, the following topics are presented:
- What is a Sim App? And how can they help DaDT analysts?
- StressCheck’s COM API
- Sim App Case Studies for DaDT
- Live Sim App Demo
WATCH THIS WEBINAR
Part 1: E2E Demo, Overview of LEFM, FEA-Based Beta Factors
Part 2: Sim Apps, StressCheck COM API, Sim App Demo
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“A screening of existent commercial and non-commercial tools was carried out in respect to their fracture mechanics capabilities, their design abilities, implementation as well as their complexity. Although, there are many software possibilities, only those within the reach of the author were evaluated. This resulted in the selection of the commercial tool StressCheck. The assessment of crack propagation on compact tension and two stringer specimens governed by the Paris and Forman regimes was satisfactory compared with experimental results using the material data from simple standard specimens.”
Lloren Llopart Prieto (EADS)
Doctoral Thesis, "Modelling and analysis of crack turning on aeronautical structures"