HyperSizer Stress Reports

HyperSizer generates Microsoft Word-based material stress reports on all aspects of your project. This technical report includes margins-of-safety, material properties, design-to loads, optimum design dimensions, etc. You can select what type of data to be included in your document using the stress report form to be used in studies and projects. An engineering report is created based on your specifications that is easy to share, contributing to a collaborative work environment - excellent for Structural Engineers. The stress reporting capability includes sample MS calculations with your actual project data used in the equations for each unique failure modes:  such as composite ply failure criteria, panel buckling, crippling, local buckling, metal strength checks, sandwich wrinkling, NASA SP8007 panel knockdown,  bolted joints, and bonded joints.

This composite and laminate analysis reporting documentation will assist engineers throughout the lifecycle of aerospace testing. Excellent for FAA Certification, this stress software works with FEA to provide complete failure analysis for an airframe. Currently, HyperSizer is used for stress calculations and stress analysis for the composite crew module testing by NASA.

Reports are also available in HTML and can be posted on a web site for ease of distribution.

Click here to download and view a sample stress report.

HyperSizer Stress Report Sample (PDF)