- Design of single-layer or laminated glass as well as gas layer insulating glass
- design of curved glass
- Option to select either local calculation without regard to the influence of a surrounding structure, or global calculation with regard to the influence of an entire structure
- Calculation of limit stresses according to DIN 18008:2010-12 or TRLV:2006-08
- Assignment of loads to load duration classes
- Extensive material library including all common glass, foil, and gas types in compliance with the DIN 18008:2010-12, E DIN EN 13474 standards, and the TRLV:2006-08 regulation
- Optional consideration of shear coupling of layers
- Consideration of climatic loads
- Calculation according to the linear static analysis or nonlinear analysis according to the large deformation analysis. analysis
- Stress analysis, ultimate limit state design, serviceability limit state design
- Graphical representation of all results in RFEM
- Possibility to filter results and color scales in result tables
- Direct data export to MS Excel
RF-GLASS | Features

The limit stresses in RF‑/STEEL can be user-defined for each thickness range.

The deformations of the FE nodes are always the first result of an FE calculation. It is possible to calculate strains, internal forces, and stresses based on these deformations and the stiffness of the elements.

This article explores the importance of considering joint-structure interaction in modeling and design and how to do it in RFEM 6.
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This article provides a comprehensive overview of essential seismic analysis methods, explaining their principles and applications, as well as the scenarios in which they are most effective

- General stress analysis
- Automatic import of internal forces from RFEM/RSTAB
- Complete graphical and numerical results of stresses and stress ratios integrated in RFEM/RSTAB
- Wide range of customization options for graphical output
- Flexible design in multiple design cases
- Clearly arranged result tables for a quick overview after the design
- High productivity due to the minimal amount of input data required
- Flexibility due to detailed setting options for basis and extent of calculations

- Cross-section optimization
- Transfer of optimized sections to RFEM/RSTAB
- Design of any thin-walled cross-section from SHAPE-THIN
- Representation of a stress diagram on a section
- Determination of normal, shear, and equivalent stresses
- Stress results of individual internal forces types
- Detailed representation of stresses in all stress points
- Determination of the largest Δσ for each stress point (for example, for fatigue design)
- Colored display of stresses and design ratios for a quick overview of the critical or oversized zones
- Parts lists and quantity surveying

- Determination of principal and basic stresses, membrane and shear stresses, as well as equivalent stresses and equivalent membrane stresses
- Stress analysis for structural surfaces including simple or complex shapes
- Equivalent stresses calculated according to different approaches:
- Shape modification hypothesis (von Mises)
- Shear stress hypothesis (Tresca)
- Normal stress hypothesis (Rankine)
- Principal strain hypothesis (Bach)
- Optional optimization of surface thicknesses and data transfer to RFEM
- Serviceability limit state design by checking surface displacements
- Detailed results of individual stress components and ratios in tables and graphics
- Filter function for surfaces, lines, and nodes in tables
- Transversal shear stresses according to Mindlin, Kirchhoff, or user-defined specifications
- Parts list of designed surfaces

In order to facilitate the data input, surfaces, members, sets of members, materials, surface thicknesses, and cross-sections are preset. It is possible to select the elements graphically using the [Select] function. The program provides access to the global material and cross-section libraries.
Load cases, load combinations, and result combinations can be combined in various design cases.
The combination of surface and member elements and separate designs allows you to model and analyze only critical parts, such as frame joints, using surface elements. The other parts of the model can be designed using member analyses.
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