The Laminate Cutout Analysis Tool (LCAT) is a Smart Engineering Simulation App providing a means to compute the strain distribution around a circular, elliptical, or racetrack cutout in a composite plate subjected to biaxial and shear loading. Additionally, LCAT determines the margin of safety for strain and the orthotropic strain concentration factor.
Laminate Cutout Analysis Tool
From the simple and intuitive interface, LCAT automatically builds, solves, and post-processes a Planar StressCheck finite element mesh of the desired laminated cutout shape/orientation and provides solution verification feedback.
Key Features and Advantages
- Solutions obtained with StressCheck, verified by p-extension.
- Built-in Results Viewer provides dynamic viewing of the FE mesh, the strain fringe contours and the strain directions.
- Supports US and SI units.
- Modeling approach validated with experimental results.
- Automatic computation of the laminate properties using CLPT given the lamina material and stacking sequence.
- The strain distribution around a cutout in the laminate composite being prepared for a repair.
- Margin of Safety calculation for the unrepaired cutout before sizing the repair patch.
- A simple and intuitive user interface allows input engineering data in pre-defined templates with step by step validation feedback.
Looking for Resources?
Recent News & Events
Quick Links
Testimonials
-
“A screening of existent commercial and non-commercial tools was carried out in respect to their fracture mechanics capabilities, their design abilities, implementation as well as their complexity. Although, there are many software possibilities, only those within the reach of the author were evaluated. This resulted in the selection of the commercial tool StressCheck. The assessment of crack propagation on compact tension and two stringer specimens governed by the Paris and Forman regimes was satisfactory compared with experimental results using the material data from simple standard specimens.”
Lloren Llopart Prieto (EADS)
Doctoral Thesis, "Modelling and analysis of crack turning on aeronautical structures"