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High cycle fatigue prediction methodology for fiber reinforced laminates for aircraft structures in CROR environment - development and validation
Date de clôture : 2 juin 2016  

 Fabrication industrielle
 Horizon Europe
 Design industriel

Topic Description
Specific Challenge:

For the design of airframe structure regions facing CROR blades, the reinforcement of CFRP has to be laid out dedicatedly in terms of fatigue resistance. Fatigue shall be described by appropriate models in simulation and verified in correlated testing. For the full topic description see the Call Text Document (Annex of Workplan) published with this call.

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