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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
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    • Dictionary & Terms
  • Resources
    • Browse Our Resource Library
    • White Papers
    • Case Studies
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    • StressCheck Tutorials

AFRL CAI Success Story

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AFRL CAI Success Story

AFRL CAI Success Story

Abstract: The two directorates, Boeing, Lockheed Martin, Northrop Grumman, and Bell Helicopter make up the CAI team. The team developed and enhanced finite element software for analysis of composite structures. The StressCheck analysis tool shows a significant improvement in bonded and co-cured joint strength prediction capabilities compared to finite element analysis tools currently on the market.

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AFRL-CAI-Success-Story_Aug2004.pdf - 978.66 KB

Related Content:

  • CAI: Transitioning Advanced Aerospace Technologies Through Cost and Risk Reduction
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  • Structural Analysis Software Tool Transitions Across DoD and the Commercial Marketplace
  • Application Brief: Detailed Analysis of Bonded Repairs
  • ASIP 2018 Training – Modeling Fastened Connections: Hierarchic Approaches Discussion and Demo


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Testimonials

When performing parametric structural analysis, ESRD’s p-element StressCheck FEA software is always my preferred choice due to the excellent solution quality, parametric framework, and superior computational efficiency. In fact, I recently used StressCheck to generate stress intensity factors along a parametrically defined elliptical crack-tip across 3,000 unique geometric configurations. Considering multi-body contact was present and all simulations were performed using a laptop, this was a task well suited for StressCheck.

Dr. Lee Zambino, Researcher, Villanova University

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