Through StressCheck Tool Box you can access smart applications designed for your specific requirements by expert analysts. These are tools that help you improve your designs efficiently, utilizing the latest developments in CAE in a user-friendly environment, with built-in documentation, designed for designers, engineers and analysts.
StressCheck Tool Box
The StressCheck Tool Box (SCTB) is a 64-bit stand-alone, Windows-based application which provides a robust, easy to use framework for solving common, but inherently challenging, engineering problems. The current target audience for SCTB applications is engineers who are not experienced in FEA but have a demand for repetitive, but high-quality, solutions in the area of fastened connections. Fully supports Windows 7, 8 and 10.
Key Features and Advantages
- No FEA or StressCheck experience is necessary to successfully run SCTB applications.
- Solutions may be exported and opened in StressCheck Professional.
- Does not require an existing installation of StressCheck to operate.
- Simple to use interface requires minimal training to be productive.
- All applications support SI and US Customary units.
SCTB Applications
Our Single Fastener Analysis Tool (SFAT) provides accurate computation of the joint stiffness, plate stresses, and fastener loads for single or double shear lap joints connected by a single fastener.
Our Multi-Fastener Analysis Tool (MFAT) provides effortless modeling of single or double shear joints, including lap joints, splice joints, and doublers (with or without a repair cutout). MFAT supports metallic and composite plates,and allows for any number of fasteners with neat fit, interference fit or clearance fit.
Our Laminate Cutout Analysis Tool (LCAT) computes 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.
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Testimonials
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“Through the use of StressCheck the A-10 Aircraft Structural Integrity Program’s (ASIP) Analysis Group is able to model more accurately the physics of fatigue crack propagation in critical aircraft structure. Through this tool we are able to model, analyze and predict failure of aircraft structure and then develop crucial inspection and maintenance planes to ensure the safety and sustainability of our nations 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.”
SWRI Research Engineer
Southwest Research Institute