Checking date: 31/12/2017

Course: 2017/2018

Propulsion systems performance and design
Study: Master in Aeronautical Engineering (296)

Coordinating teacher: DISCETTI , STEFANO

Department assigned to the subject: Department of Bioengineering and Aerospace Engineering

Type: Compulsory
ECTS Credits: 6.0 ECTS


Students are expected to have completed
Competences and skills that will be acquired and learning results.
Description of contents: programme
Learning activities and methodology
Assessment System
  • % end-of-term-examination 60
  • % of continuous assessment (assigments, laboratory, practicals...) 40
Basic Bibliography
  • Mattingly J.D., Heiser W.H., Pratt D.T.. Aircraft Engine Design. AIAA EDUCATION SERIES J. S. Przemieniecki Series Editor-in-Chief. 2003
Additional Bibliography
  • Boyce M.P.. Gas Turbine Engineering Handbook. Butterworth-Heinemann. 2011
  • Kerrebrock J.L.. Aircraft Engines and Gas Turbines. The MIT Press. 1992
  • Oates G.C.. Aerothermodynamics of Aircraft Engine Components . AIAA. 1985
  • Walsh P.P., Fletcher P.. Gas Turbine Performance. Blackwell Science Inc. 2004
  • . The Jet Engine. Rolls Royce Technical Publications. 1996

The course syllabus and the academic weekly planning may change due academic events or other reasons.