Doctoral Student on the Aerodynamic Behavior of the Compressor" - Dortches, NC, United States - Horizon Group
Description
MTU Aero Engines is a company that develops, manufactures, distributes, and supports civilian and military aircraft and helicopter engines, as well as industrial gas turbines.
Our key to success lies in creating engines for the aviation of tomorrow - more efficient, environmentally friendly, and quieter.
With over 11,000 employees, we are present worldwide and based in Germany. Join our dedicated team at our location inMunich **as a
Doctoral Candidate in Aerodynamic Behavior of Compressors with Inlet Disturbances (all genders)
Reference Number - AEAV 716
In the design of a compressor, a homogeneous inflow is typically assumed.
However, a curved inlet, which may be necessary due to space constraints, or crosswinds during flight can lead to an inhomogeneous inflow to the compressor.
This can have a negative impact on the efficiency and stability of the compressor. To evaluate this influence using CFD simulations, complex and time-consuming unsteady models are usually required.A faster alternative is the use of analytical methods, which model the aerodynamic behavior of disturbed and undisturbed compressor sectors and determine the overall effect on the compressor through combined calculation of the individual sectors.
The aim of this doctoral thesis is to further develop calculation methods for evaluating compressor behavior with disturbed inflow, as well as to investigate the aerodynamic coupling between compressor and inlet flow.
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