| KEYWORD |
Area Engineering
Numerical simulation and optimization of a transition duct coupled with a constant volume combustor designed for propulsion
Reference persons DANIELA ANNA MISUL, SIMONE SALVADORI
External reference persons PANAGIOTIS GALLIS
Thesis type SIMULATION
Description The activity consists in the numerical simulation of a geometry placed at the exhaust of a constant volume combustor for aeronautical applications, experimentally tested at ENSMA (FR). The student will have to support the research group in the preparation and execution of the simulation with the ultimate aim of characterizing the functioning of the existing geometry with respect to a matrix of boundary conditions, comparing the obtained results with the available experimental data. Downstream of the validation phase, it will be possible to carry out a first optimization of the geometry by including a high pressure compartment (if possible).
Required skills Operation of gas turbines, compressible fluid dynamics, computational fluid dynamics
Deadline 31/12/2022
PROPONI LA TUA CANDIDATURA