Standard NAFEMS Benchmark Solutions Coming Soon
In the coming weeks, ESRD will publish our first set of FEA-based numerical simulation results from “The Standard NAFEMS Benchmark Solutions”. Learn more […]
In the coming weeks, ESRD will publish our first set of FEA-based numerical simulation results from “The Standard NAFEMS Benchmark Solutions”. Learn more […]
We’ve uploaded more than a dozen NEW StressCheck tutorial videos […]
We have added high-resolution StressCheck showcase videos to our resource library. These videos are intended to demonstrate StressCheck’s suite of...
In this video demo, we show how to easily define a subsurface residual stress (SRS) profile, due to shot peening or another...
“The addition of incremental theory of plasticity in StressCheck has greatly improved our ability to accurately predict the fatigue life of joints with interference fit fasteners and cold worked holes. This ability is especially important, not only in support of maintaining aging aircraft but also in analyzing some of the new cold working techniques that have been introduced in recent years.
Prior to this implementation, analysts often relied on closed-form approximations or simple factors that were often overly conservative and sometimes even unconservative when used in life prediction. Now, not only can we more accurately predict residual stresses in these complex structural joints, but we can also do so in a timely manner given the modeling and analysis efficiency that exists with a p-version FEA code such as StressCheck.”
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