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  • About
    • Who We Are
    • Partners & Providers
    • News & Events
    • The ESRD Blog
    • Careers
    • Contact Us
  • Applications
    • What We Solve
    • Detailed Stress
    • Composites
    • Fracture Mechanics
    • Residual Stress
    • Sim Apps
  • Products
    • What We Develop
    • StressCheck Professional
      • StressCheck Core
      • Solvers
      • Advanced Modules
      • Utilities
      • Academic Licensing
    • StressCheck Apps
      • CAE Handbook
      • StressCheck Tool Box
    • Product Updates
  • Support
    • How We Can Help
    • Training
    • Webinars
    • Quick Start Guide
    • Help Documentation
    • Software FAQ’s
  • Simulation
    • How We Simulate
    • Benchmarks
    • Simulation Governance
    • History of FEA
    • Dictionary & Terms
  • Resources
    • Browse Our Resource Library
    • White Papers
    • Case Studies
    • Product Demos
    • StressCheck Tutorials

Advanced Modules

Home ProductsStressCheck ProfessionalAdvanced Modules

StressCheck Advanced Modules

StressCheck Professional has advanced modeling capabilities in the areas of composites, fracture, residual stress and more. These are the StressCheck Advanced Modules, each module independently licensed as add-on modelers. Many of the features in these modules may even be combined together in a single model for more sophisticated FEA needs.

For example, an engineering application involving multi-body contact, plasticity, composites and fracture mechanics (such as for a bolted/bonded doubler repair over a cracked aluminum skin) can be efficiently simulated in StressCheck via the Composites and Fracture Mechanics modules, respectively.

  • Composites
  • Fracture Mechanics
  • Bulk Residual Stress
  • Subsurface Residual Stress

Composites

3D ply-by-ply analysis with the Composites Module, enhanced through our Automatic Laminate Builder, allows you to conveniently estimate the interlaminar stresses and strains required to accurately predict interlaminar failure or assess the structural integrity of the joint.

As a result, the Composites Affordability Initiative (CAI) unanimously selected the StressCheck Composites module to “replace as well as radically improve existing industry software currently used for bonded joints.”

Countersunk fastened joint with ply-by-ply stack plate.

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Fracture Mechanics

Once you solve a fracture mechanics problem with StressCheck, you won’t want to use another FEA tool for that purpose again. You will experience ease of use, realize superconvergence and receive high definition feedback information you need to guarantee the reliability and accuracy of the computed stress intensity factors (SIF) and energy release rates (ERR).

“Through [StressCheck] we are able to model, analyze and predict failure of aircraft structures and then develop crucial inspection and maintenance plans to ensure the safety and sustainability of our nation’s warplanes. Without the analysis capability provided to us through StressCheck we would not be able to provide accurate assessments of the A-10 structure to top USAF leadership.” – Southwest Research Institute Manager

Mixed Element Crack Front Automesh with AUTO Integration Radius for SIF Extraction

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Bulk Residual Stress

Many manufacturing or metal forming processes (such as cold working of holes) can induce residual stress throughout the volume of material. These bulk residual stresses (BRS) can significantly influence fatigue life, structural stability, failure loads, and distortion after machining. StressCheck allows such stresses, or the corresponding eigenstrains, to be included in linear analyses with industry-leading solution quality assurance procedures.

Figure 1. BRS process for computing distortion of a part due to forming.

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Subsurface Residual Stress

The effects of residual stresses can be beneficial, as in life extension by cold working, or detrimental, requiring reworking or rejecting manufactured parts. Reliably simulating effects of residual stresses is challenging due to extreme stress gradients. With the technology in StressCheck, representing rapidly changing stresses over short distances is a breeze.

Figure 1. This work was sponsored by the Air Force Research Laboratory SBIR topic: “Efficient Shaping or Reshaping of Complex 3D Parts Using Engineered Residual Stress”.

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Testimonials

  • “As frequent StressCheck users we rely on the capabilities and reliability of the program to complete our everyday jobs ensuring safe reliable flights of our aircraft. The layout of the program and documentation allow for a quick learning process and the support ESRD offers is second to none. They take the time to answer the most basic questions as well as working through complex problems to ensure the proper validation of results. The effort they make in satisfying their users needs increase the reliability, functionality, and capability of this great program.”

    USAF Engineer
    Hill Air Force Base

Testimonials

“As frequent StressCheck users we rely on the capabilities and reliability of the program to complete our everyday jobs ensuring safe reliable flights of our aircraft. The layout of the program and documentation allow for a quick learning process and the support ESRD offers is second to none. They take the time to answer the most basic questions as well as working through complex problems to ensure the proper validation of results. The effort they make in satisfying their users needs increase the reliability, functionality, and capability of this great program.”

USAF Engineer, Hill Air Force Base

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