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Course: 2020/2021

Turboprop Design

(14177)

Bachelor in Aerospace Engineering (Plan: 421 - Estudio: 251)

Coordinating teacher: RAIOLA , MARCO

Department assigned to the subject: Bioengineering and Aeroespace Engineering Department

Type: Electives

ECTS Credits: 3.0 ECTS

Course: 4º

Semester:

Requirements (Subjects that are assumed to be known)

- Fluid Mechanics - Thermal Engineering - Aerodynamics - Aerospace Propulsion

ObjectivesFurther information on this link

The goal of this course is that the student acquires a basic knowledge of aircraft propellers and turbo-prop engines.

Description of contents: programme

Introduction to propulsion systems - Review of basic principles of propulsion - Overview of different aeronautic engines The Propeller - Geometry and characteristics of propellers - Momentum and blade element theory - Propeller propulsive efficiency - Propeller noise - Propeller testing - Design of optimum propellers Turboprop and Turboshaft Engines - Cycle analysis of conventional-free-turbine turboprop engine - Optimization of turboprop engines - Installation issues - The impact on regional aviation - The Unducted Fan

Learning activities and methodology

- Theory sessions. - Problem sessions. - Computer sessions. - Lab-sessions.

Assessment System

1)	To have a MINIMUM mark of 4.0/10 in the end-of-term exam;
2)	To have a MINIMUM  overall mark of 5.0/10 (weighing 25% the end-of-term exam mark and 75% the mark of the continuous evaluation).

% end-of-term-examination 25
% of continuous assessment (assigments, laboratory, practicals...) 75

Basic Bibliography

D.R. Greatrix. Powered Flight. The engineering of Aerospace Propulsion. Springer. 2012
J. L. Kerrebrook. Aircraft Engines and Gas Turbines. The MIT Press. 1992
R. Von Mises. Theory of flight. Courier Dover Publications. 2012

The course syllabus may change due academic events or other reasons.