The following is a typical stress history of the normal stress on the composite wing spar during a flight between London and Rome, which was recorded by Digital Twin. It is used to evaluate the assessment of fatigue damage over all different phases of flight and to predict the remaining life.
1) Residual stress prediction during manufacturing (e.g., curing, cooling, lay-up processes)
2) Defect and fatigue damage monitoring for performance assessment and durability
3) Cloud-native accessibility, allowing secure, collaborative data access from anywhere
4) Seamless integration into digital product development pipelines
Sumandra is proud to partner with CETIM - France, CCQ Tech, Arts University Bournemouth and Indian Institute of Technology - Guwahati in Twinalyzing the structure.