University of Liege | Version française
Study programmes 2013-2014Last update : 13/05/2014
AERO0023-1  Aircraft design

Duration :  30h Th, 30h Pr
Number of credits :  
Master in Aerospace Engineering, research focus, 1st year5
Master in Aerospace Engineering, research focus (Thrust), 1st year5
Master in Aerospace Engineering, Professional Focus (Management), 1st year5
Lecturer :  Grigorios Dimitriadis, Ludovic Noels
Language(s) of instruction :  
French language
Organisation and examination :  
All year long
Course contents :  
During these classes, the students will learn about the integrated design of an aircraft. Indeed, each technical field is seen as a sub-system interacting with the others.
Therefore, the organisation is as follows. An introductive talk describes, through history, these interactions, and a concluding talk will introduce the project of designing an aircraft.
Between these two classes, professors will introduce the concepts of
  • Aerodynamics
  • Structures
  • Propulsion (flow and mechanical design)
  • Performances
  • Stability
  • Aeroelasticity
Learning outcomes of the course :  
A the end of the class the student will have acquired the methodology to conduct a conceptual design in aeronautics. In particular he will be able to achieve the conceptual design of a jetline.
Prerequisites and co-requisites/ Recommended optional programme components :  
Basic knowledge in
  • Solid mechanics
  • Fluid mechanics
Planned learning activities and teaching methods :  
Industrial partners are invited to give lectures during which they illustrate the theoretical concepts with realizations of aeronautic companies.
Mode of delivery (face-to-face ; distance-learning) :  
Face to face
Recommended or required readings :  
  • Aircraft Design: Synthesis and Analysis, Ilan Kroo, Stanford University, http://adg.stanford.edu/aa24 /AircraftDesign.html
  • Synthesis of Subsonic Airplane Design, Egbert Torenbeek, Delft University Press, Kluwer Academic Publishers, The Netherlands, ISBN 90-246-2724-3, 1982
  • Aircraft Design: A Conceptual Approach, Daniel P. Raymer, Ph.D. AIAA Education Series, Reston, VA, 2012 ISBN 978-1-60086-911-2
Assessment methods and criteria :  
The evaluation is based on a project, which consists in the pre design of a turbojet. This project will be presented in front of the professors and the classmates.
Participation to the talks of the invited lecturers and to the project presentations is mandatory.
Work placement(s) :  
Organizational remarks :  
Classes are taught during first term; project is accomplished during the 2 terms and is presented during the 2nd term.
Contacts :  

Items online :  
Lectures on WebCt
Slides on


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