Looking for a webinar to watch during lunch tomorrow? Register here for our “Durability and Damage Tolerance (DaDT) Best Practices Webinar” @ 1:00 pm EST. We hope to see you hop on!
Looking for a webinar to watch during lunch tomorrow? Register here for our “Durability and Damage Tolerance (DaDT) Best Practices Webinar” @ 1:00 pm EST. We hope to see you hop on!
Recently at ASIP 2022 in Phoenix, AZ, ESRD provided a 2-hour training course titled “Best Practices for the Modeling and Analysis of Bonded Doubler Repairs”, presented a technical paper titled "DTA of Bonded Repairs on the Wing Skin of the C-130 Using Finite Elements", chatted with "patients" at the StressCheck Clinic, and exhibited at our captivating booth inside the Sheraton Phoenix Hotel & Conference Center. We are also planning a webinar for February 7, 2023 titled "What's New and Improved in StressCheck Professional". We hope you can attend this "must-see" event! Read the summary of conference events, view the ASIP training course content (including the presentation and demo videos), and register for our upcoming webinar.
Good news, everyone! We are working hard to finalize StressCheck Professional v10.5, and we'd like to share some of the latest features and enhancements users can expect to see in the next release (anticipated for Spring 2019)
Learn how Simulation Governance was introduced, how it came to be one of the Big Issues of NAFEMS, and how ESRD's leadership and other world-renowned simulation experts are using this powerful function for enhancing reliability of modern numerical simulation [...]
“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.”
© 2026 · Engineering Software Research & Development, Inc. | Terms & Conditions | Privacy & Cookie Policy | Software License Agreement | Software Maintenance and Technical Support Policy
Leave a Reply
We appreciate your feedback!
You must be logged in to post a comment.