HOW CAN WE HELP?
Using numerical and analytical methods in aircraft structural joint and assembly design enables faster certification, lower costs, greater safety, and effective solutions for non-standard analyses. We offer unique know-how and methods, verified by dozens of Czech and foreign development programs, detailed knowledge of certification methods (including fault conditions), and reduced experimental requirements through verified simulation models and a database of material characteristics.
WE OFFER
- Complex solutions for strength and durability of materials and structures
- Analysis of composite structures, incl. modeling of degradation processes and their optimization
- Calculations of stress and strain distribution, limit states, stability, buckling strength
- Simulation and calculation of fatigue crack propagation and service life assessment
- Topological, strength, stiffness, and weight optimization of structures
- Multi-physical simulation (acoustics, electromagnetism, FSI – Fluid Structure Interaction)
- Crash analysis and simulation (high-speed impact)
- Rotor dynamics (complex modes, critical speed, Campbell diagram)
- Modeling and simulation of dynamic systems