Ingénieur aéroélasticité experimentale voilures tournantes 18 Mois H/F, Châtillon
Missions
Integrated into the "Aéroélasticité et Dynamique des Structures Expérimentales (ADSE)" unit, you actively participate in projects to characterize the dynamic behavior of structures or to analyze aeroelastic phenomena mainly through experimental approaches.
You primarily contribute to studies concerning rotating systems covering a wide domain of applications (helicopter blade, propeller, compressor inlet, new architecture fan, etc.) combining modeling, simulation and experimentation.
In laboratory testing campaigns, on bench or in wind tunnel, you participate in all phases, from the creation of simplified structural models for design, numerically simulating aeroelastic behavior to analyzing test data.
You also contribute to the development and validation on bench of measurement methodologies applicable to rotating systems such as identifying dynamic behavior in rotation.
Your work is part of national, European or internal research projects, conducted in close collaboration with other engineers of the unit, the DAAA department, or external partners. You must organize your work to deliver results within imposed deadlines and synthesize main results into technical presentations and reports in French and English.
Profile
Engineer and/or Doctor, with a strong interest in mechanics and experimental domain.
Knowledge in structure design and modeling (CAD, FEM) and proven experience in vibratory dynamics.
Basic knowledge of aeroelasticity or signal processing appreciated.
Proven experience in a programming language.
Teamwork mindset.
Excellent written communication and oral presentation skills.
Environment
The Aero-dynamics, Aeroelasticity, Acoustics Department (DAAA) prepares technological responses for industry to improve aerodynamics, aeroelasticity and acoustic performance of aircraft.
The ADSE unit conducts experimental studies dedicated to characterizing and identifying the dynamic behavior of structures, and analyzing aeroelastic phenomena.
#J-18808-Ljbffr