Educational guide
IDENTIFYING DATA 2022_23
Subject JET ENGINES Code 00710333
Study programme
0710 - GRADO EN INGENIERÍA AEROESPACIAL
Descriptors Credit. Type Year Period
6 Compulsory Third Second
Language
Castellano
Prerequisites
Department ING.MECANICA,INFORMAT.AEROESP.
Coordinador
LOPEZ RODRIGUEZ , DEIBI
E-mail dlopr@unileon.es
ddomf@unileon.es
Lecturers
DOMINGUEZ FERNANDEZ, DIEGO
LOPEZ RODRIGUEZ , DEIBI
Web http://
General description
Tribunales de Revisión
Tribunal titular
Cargo Departamento Profesor
Presidente ING.MECANICA,INFORMAT.AEROESP. PEREZ GARCIA , HILDE
Secretario ESCAPA GARCIA , LUIS ALBERTO
Vocal ING.MECANICA,INFORMAT.AEROESP. GONZALO DE GRADO , JESUS
Tribunal suplente
Cargo Departamento Profesor
Presidente ING.MECANICA,INFORMAT.AEROESP. BARREIRO GARCIA , JOAQUIN
Secretario ING.MECANICA,INFORMAT.AEROESP. MARTINEZ PELLITERO , SUSANA
Vocal ING.MECANICA,INFORMAT.AEROESP. RODRIGUEZ MATEOS , PABLO

Competencias
Code  
A17712
A17713
B958
B960
B961
B5474
B5476
C1
C2
C4

Learning aims
Competences
A17712
A17713
B958
B960
B961
B5474
B5476
C1
C2
C4
A17712
A17713
B958
B960
B961
B5474
B5476
C1
C2
C4

Contents
Topic Sub-topic
Bloque I: INTRODUCTION TO JET ENGINES AND THEIR ARCHITECTURES Tema 1: JET ENGINE INTRODUCTION
Historical introduction and jet engine evolution

Tema 2: ARCHITECTURE AND CLASSIFICATION
Jet engine classification and basic configuration
Bloque II: GENERAL EQUATIONS AND ENERGETIC ANALYSIS Tema 1: GENERAL EQUATIONS AND ENERGETIC ANALYSIS
Bloque III: REAL THERMODYNAMIC CYCLE APROXIMATIONS Tema 1: REAL THERMODYNAMIC CYCLE ANALYSIS
Ideal to real thermodynamic cycle aproximations of jet engines
Bloque IV: ENGINE COMPONENT ARCHITECTURE AND PERFORMANCE Tema 1: INTAKES
Architecture and performance

Tema 2: AXIAL COMPRESSORS
Architecture and performance

Tema 3: RADIAL COMPRESSORS
Architecture and performance

Tema 4: COMBUSTORS AND AFTERBURNERS
Architecture and performance

Tema 5: TURBINES
Architecture and performance

Tema 6: NOZZLES
Architecture and performance
Bloque V: COMPOMENT ACTUATIONS Tema 1: TURBENE AND COMPRESSOR SHAFT
Compressor-turbine matching

Tema 2: PERFORMANCE MAPS
Compressor and turbine maps

Planning
Methodologies  ::  Tests
  Class hours Hours outside the classroom Total hours
Problem solving, classroom exercises 20 30 50
 
Laboratory practicals 8 15 23
Personal tuition 1 0 1
 
Lecture 28 45 73
 
Mixed tests 2.5 0 2.5
0.5 0 0.5
 
(*)The information in the planning table is for guidance only and does not take into account the heterogeneity of the students.

Methodologies
Methodologies   ::  
  Description
Problem solving, classroom exercises
Laboratory practicals
Personal tuition
Lecture

Personalized attention
 
Personal tuition
Description

Assessment
  Description Qualification
Mixed tests 75%
25%
 
Other comments and second call

Sources of information
Access to Recommended Bibliography in the Catalog ULE

Basic Jack D. Mattingly, Elements of Gas Turbine Propulsion, Mac Graw-Hlll, New York, 1988
Hill & Peterson, Mechanics and Thermodynamícs of Propulsion, Addison-Wesley Reading, Massachusets, 1992

Complementary Jack D. Mattingly, Aircraft Engine Design, American Institute of Aeronautics and Astronautics, New York, 1987
Daly, Mark, Jane's Aero Engines, IHS, 2012
J.L. Montañes García, Motores de reacción y turbinas de gas, ETSI Aeronáuticos, Madrid, 2005
Rolls Royce, The Jet Englne, Rolls Royce, Derby, 1986


Recommendations

Subjects that are recommended to be taken simultaneously
THERMAL AND COMBUSTIBLE ENGINEERING / 00710334

Subjects that it is recommended to have taken before
LINEAR ALGEBRA AND GEOMETRY / 00710301
DIFFERENTIAL AND INTEGRAL CALCULUS / 00710302
AEROSPACE TECHNOLOGY / 00710312
AERODYNAMICS / 00710318
PROPULSIÓN / 00710320