The course is a continuation of MJ2241 Jet Propulsion Engines, General Course and therefore starts at an advanced level. As the nucleus of present-day aircraft engines consists of gas turbines, the course is to a large extent coordinated with the course MJ2430 Thermal turbomachinery. Propulsion of modern aircraft would not be possible without thermal turbomachines that are characterised by unrivalled power density.
The course starts with an introduction of simple calculus of one variable and turbomachine components and then the level of the course is extended to 2D and 3D analysis aspects. Important aspects such as cooling in combustion turbines, mechanical effects, material and the properties of the system are highlighted in the course and introduced in relevant contexts.
Special focus is placed on discussion of aerodynamic design of vanes for turbofan engines, as these produce the majority of thrust in propulsion of passenger aircraft.
Critical review of scientific articles will be carried out within the frame of the course to stimulate to discussions in an interdisciplinary environment. Practical assignments will be given to deepen the student's understanding of the phenomena treated in the course. A study visit to a gas turbine manufacturer or a relevant company is planned.
The course is given in English
Note: The course may not be chosen, if one follows or has taken the course MJ2430 Thermal turbomachinery.