Hill Engineering and ESRD have executed a joint marketing agreement to collaboratively promote the combined use of our software tools Broad Application for Modeling Failure (BAMF) and StressCheck® Professional, respectively, for the engineering applications of fatigue and damage tolerance analysis.
This past week at ASIP 2019, ESRD provided a training course titled “Automated 3D Crack Beta Curve Development via Smart Sim Apps”, chatted with ASIP attendees, provided a StressCheck® Clinic, and exhibited at our booth.
Read the summary of events and download the ASIP training course presentation and beta factor Sim Apps!
ESRD, Inc. will be exhibiting and providing a training course on automated 3D crack beta curve development via FEA-based #SimApps at the ASIP Conference 2019 in San Antonio, TX from December 2-5, 2019.
On July 29, 2019 a joint webinar on the the importance of Simulation Governance in FEA-based Sim App development & deployment, titled “Democratization of Simulation Governance-Compliant Sim Apps”, was provided by ESRD’s Brent Lancaster and Rev-Sim’s Malcolm Panthaki. In case you missed it, the webinar recording is now available!
On July 17, 2019 a joint webinar on the latest developments in FEA-based 3D crack growth simulation, titled “3D Crack Growth Simulation: Advancements & Applications”, was provided by ESRD’s Brent Lancaster, LexTech’s James Harter and Hill Engineering’s Joshua Hodges. In case you missed it, the webinar recording is now available!
Want to learn from the experts in FEA-based Simulation Application (Sim App) development for standardization & automation of complex engineering analysis tasks, such as 3D fatigue crack growth, 3D ply-by-ply laminated composite analysis or other challenging applications you’d like to safely put into the hands of non-experts?
This July, ESRD will be partnering with several industry leaders to provide not one but TWO stimulating webinars on the latest in FEA-based Sim App development.
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“At DST Group, we have effectively used StressCheck® over the last 10 years to determine accurate stress intensity factors. The results have been used to improve our residual strength and structural life estimates for aircraft in service with the Royal Australian Airforce, including C-130, P-3C and F/A-18 A/B. We have found it to be extremely easy to use and a very versatile code with which to create parametric models.
We have recently used StressCheck® to obtain improved stress intensity factor solutions (Improved stress intensity factors for selected configurations in cracked plates and Improved stress intensity factors for a single corner crack at a loaded fastener hole) for five key generic configurations. These transferable parametric results have been published externally. One specific example is the non-linear contact analysis of a cracked, filled fastener hole, with both fastener and remote plate loading.”
Dr. Manfred Heller, HeadStructural & Damage Mechanics, DST Group