GAS TURBINE COMBUSTORS

Course objectives

Knowledge and understanding Knowledge of the main types of aeronautical combustors, the chemical-physical properties of fuels, pollutant emissions, theories and mathematical and numerical models used to predict performance and environmental impact, as well as innovative and low-impact architectures and fuels environmental. Applying knowledge and understanding Ability to perform a rough sizing of the aeronautical combustor and to predict its performance, using calculation tools produced by the students themselves during the group work. The training objectives are pursued using classroom exercises and reviews of work in progress. The assessment of the acquired skills occurs at the same time as that of the knowledge during the reviews and in the course. Autonomy of judgment (making judgments) Skills are acquired through lectures, exercises in the classroom and for carrying out group work. Verification of knowledge takes place through individual tests and through written group reports which at the same time ensure and promote the acquisition of the ability to communicate effectively in written and / or oral form. Communication skills Ability to work in a group, to present the results of group work with presentations and short technical reports. Ability to learn (learning skills). Knowledge characterizing the systems engineer of aeronautical propulsion, with particular attention to issues related to the design and numerical modeling techniques of a combustion chamber and emission control.

Channel 1
PIETRO PAOLO CIOTTOLI Lecturers' profile

Program - Frequency - Exams

Course program
The course deals with the design and environmental impact of gas turbines combustion chambers for aeronautical applications. Particular attention is devoted to the combustion chamber numerical modelling techniques. The topics covered by the course are listed below. Chapter 1 Introduction Chapter 2 Combustion chambers design Chapter 3 Review of thermodynamics of reacting mixtures Chapter 4 Aviation fuels Chapter 5 Fundamentals of turbulent flows and turbulent combustion modelling Chapter 6 Fundamentals of spray dynamics and spray modelling Chapter 7 Pollutants and contaminants formation and control
Prerequisites
The knowledge that the student must have at the beginning of the teaching activities, in order to understand their contents and to achieve the learning objectives of the teaching, are the following: The knowledge of thermodynamic cycles of interest in aeronautical propulsion (Carnot cycle, Brayton-Joule cycle, ideal and real cycles) is indispensable. Knowledge of the performance parameters of an aeronautical propulsion system (thrust, specific consumption, ...) is indispensable. It is important to know the basic concepts of thermodynamics and chemistry of organic compounds. It is useful to have knowledge of the basic concepts of aerodynamics of wing profiles and bluff bodies. It is useful to know the basic concepts of gasdynamics of compressible flows including the jump relationships for normal and oblique shocks.
Books
Dilip R. Ballal, Arthur H. Lefebvre Gas Turbine Combustion: Alternative Fuels and Emissions, Third Edition, CRC 1983, Taylor and Francis Arthur H. Lefebvre Vincent G. McDonell, Atomization and Sprays, Second Edition, CRC 2017, Taylor and Francis T. Poinsot, D. Veynante, Theoretical and Numerical Combustion, R.T. Edwards, Inc., 2005 C.K. Law, Combustion Physics, Cambridge University Press 2010 Lecture notes: http://dma.dima.uniroma1.it:8080/STAFF2/
Teaching mode
The course will be delivered through frontal lessons in presence and/or in telematic mode. The course materials and all communication between teacher and student will be managed through the Goggle Classroom platform which can be accessed using any internet browser. All interested students are therefore invited to register on the Goggle Classroom page of the course of interest using their INFOSTUD credentials. Students who enroll in the course will receive an email notification of the lesson calendar which will be provided in telematic mode until otherwise specified.
Frequency
The course will be delivered through frontal lessons in person and/or, in exceptional cases, in telematic mode. The course materials and all communication between teacher and student will be managed through the Google Classroom platform, which can be accessed using any internet browser.
Exam mode
The assessment includes a written test, an oral test, and the evaluation of a group paper produced during the course. The written test consists of open-ended questions. The written test lasts 3 hours; you are not allowed to use any material during the test. The projects will be valued by adding 0/30 to 3/30 to the mark obtained after the written and oral tests. The delivery of the paper is a pre-requisite to take the written test.
Bibliography
Dilip R. Ballal, Arthur H. Lefebvre Gas Turbine Combustion: Alternative Fuels and Emissions, Third Edition, CRC 1983, Taylor and Francis Arthur H. Lefebvre Vincent G. McDonell, Atomization and Sprays, Second Edition, CRC 2017, Taylor and Francis T. Poinsot, D. Veynante, Theoretical and Numerical Combustion, R.T. Edwards, Inc., 2005 C.K. Law, Combustion Physics, Cambridge University Press 2010 Lecture notes: http://dma.dima.uniroma1.it:8080/STAFF2/
Lesson mode
The course will be delivered through frontal lessons in presence and/or in telematic mode. The course materials and all communication between teacher and student will be managed through the Goggle Classroom platform which can be accessed using any internet browser. All interested students are therefore invited to register on the Goggle Classroom page of the course of interest using their INFOSTUD credentials. Students who enroll in the course will receive an email notification of the lesson calendar which will be provided in telematic mode until otherwise specified.
  • Lesson code10592716
  • Academic year2025/2026
  • CourseAeronautical engineering
  • CurriculumModellistica e analisi per la progettazione aeronautica (percorso valido anche per il conseguimento del doppio titolo con Georgia institute of technology and Georgia tech Lorraine o per il doppio titolo Italo-portoghese )
  • Year2nd year
  • Semester1st semester
  • SSDING-IND/07
  • CFU6