Ph.D. student with prior degrees in Mechanical, Aeronautical, Aerospace Engineering, or related field. The selected individual will conduct his research in one or more of our ongoing efforts in the turbomachinery field: • Adaptive Cycle Micro-Turbofan Engine Development, • Inverted Brayton Bottoming Cycle for Hot Gas Energy Recovery, • Additively Manufactured Micro Gas Turbines, • Economic Dispatch of a Micro-Gas Turbine CHP Generator, • Cold Flow Mixing Process in Micro-Combustors. Requested Profile: • A pre-existing solid background, or a strong desire to acquire knowledge, in the following subjects is essential: Cycle Analysis, Aero-Thermal Design of Gas Turbines, Turbomachinery Aerodynamics. • Expertise in finite element / volume solvers (such as COMSOL, ANSYS, Fluent, CFX), and proficiency in MATLAB is a strong benefit. • High level of English language proficiency is desirable. • Candidates are expected to be self-motivated, hardworking and team players.
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