|SCIENTIFIC DISCIPLINARY SECTOR||ING-IND/08|
|MODULES||This unit is a module of:|
The course provides to the students the basic rules for the preliminary design of the different aero-engine components, in order to satisfy the required thrust, and the thermodynamic constrains imposed by the cycle analysis. In a second phase the operation of each component will be deeply investigated looking at the internal aerodynamics, thus highlighting the most important flow and geometrical parameters affecting the component performance.
The objective of the course is to provide students with tools for the design of the different components of an aircraft engine: engine inlet, compressor, combustor, turbine, diffuser and nozzle.
At the end of the course the student should be able to:
- perform an accurate cycle analysis of the aeroengine, identifying the boundary conditions for the design of the different components;
- design, through a preliminary procedure, each aeroengine component: intake, compressor, combustion chamber, turbine and propulsive nozzle;
- analyze in detail the aerodynamics of each component;
- apply the matching of the components in order to identify the nominal operating point of the system.
Frontal lessons will be mainly employed in the course. The basic design rules of each component will be provided. Experimental and numerical results characterizing the real operation of each component will be also shown. It is strongly suggested the participation of the student to the lessons, since the examination is driven by arguments discussed and presented during the lessons
DANIELE SIMONI (President)
FRANCESCA SATTA (President Substitute)
All class schedules are posted on the EasyAcademy portal.
The examination will be carried out by means of an oral discussion. The examination data will be provided previous appointment.
Students with SLD, disability or other regularly certified special educational needs are advised to contact the instructor at the beginning of the course to agree on teaching and examination methods that, in compliance with the course objectives, take into account the individual learning requirements.
The oral examination will allow to verify the acquired knowledge of the student regarding the operation of the different components, and how they can be optimized thanks to an increasing knowledge of the internal aerodynamics of the components, as well as in the evaluation of the capability of the student in adopting the design rules and the matching between the different components.
|16/02/2023||10:00||GENOVA||Esame su appuntamento|
|15/09/2023||10:00||GENOVA||Esame su appuntamento|