Be responsible for research and technical support into projects related to structural mechanics and aerodynamics of various propulsion systems, including UAV/VTOL Rotor systems.
Perform mechanical design and Finite Element Analysis of propulsion systems.
Liaise with the team to support experimental testing activities.
Develop knowledge and skills within TII related to the latest techniques and applications relevant to Propeller/Rotor Structural integrity and Aerodynamics, and Finite Element Analysis.
Liaise with superiors to make decisions for project development and new R&D opportunities.
Collaborate with internal and external research partners to advance the understanding of propulsion systems.
Foster a collaborative work environment and provide technical guidance to junior researchers.
Disseminate research findings through high-quality publications in prestigious scientific journals and present at conferences and workshops. Contribute to the institute's intellectual property portfolio through patents, articles, and technical reports.
Industry/ Domain: Propulsion & Space Research Center
Necessary Knowledge and Experience
Master’s degree in Aeronautical, Aerospace, Mechanical or related engineering field.
5+ years of experience in mechanical design engineering and Finite Element Analysis.
Experience in composite material simulation.
Experience in Aeroelasticity and/or Aerodynamics.
Overall adaptability to multi-disciplinary projects is required (structural mechanics, aerodynamics, testing).
Experience in ANSYS-Mechanical is preferred.
Hands-on experience is preferred.
Good knowledge of CAD software used for complex designs, preferably Catia, NX, Creo or Solidworks.
Good knowledge of algorithms and program codes (Python, C/C++, Matlab).
Must be motivated to learn and to work in a dynamic environment, thinking outside the box and helping to build a new center at TII.
Active member of a professional engineering association and international network of contacts in academia and industry will be considered a plus.