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This project focus on the analysis of different shielding configurations to protect a rear-end structure of an open rotor aircraft from an engine failure. The analysis will be performed against simple panels in the first place. The best configurations will then be studied as aircraft representative structures. Two different types of impactor will be considered from the engine failure, a metallic f ...

"The goal of the project is design and manufacture a specific test bench dedicated to give more confidence of the design in term of reliability at components level and help the user to expertise and to validate the minimum life expectation of future aircraft power electronics converters.Endurance Tests and Reliability Prediction of avionics is a critical part of the development of on-board electro ...