Educational guide
IDENTIFYING DATA 2024_25
Subject TURBOPROP ENGINES Code 00710340
Study programme
0710 - GRADO EN INGENIERÍA AEROESPACIAL
Descriptors Credit. Type Year Period
6 Compulsory Fourth First
Language
Castellano
Prerequisites
Department ING.MECANICA,INFORMAT.AEROESP.
Coordinador
LOPEZ RODRIGUEZ , DEIBI
E-mail dlopr@unileon.es
agarcg@unileon.es
Lecturers
GARCIA GUTIERREZ , ADRIAN
LOPEZ RODRIGUEZ , DEIBI
Web http://
General description
Tribunales de Revisión
Tribunal titular
Cargo Departamento Profesor
Presidente ING.MECANICA,INFORMAT.AEROESP. PEREZ GARCIA , HILDE
Secretario ING.MECANICA,INFORMAT.AEROESP. DOMINGUEZ FERNANDEZ , DIEGO
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 CMECES1 That students have demonstrated possession and understanding of knowledge in an area of study that is based on general secondary education, and is usually found at a level that, although supported by advanced textbooks, also includes some aspects that involve knowledge from the cutting edge of their field of study
C2 CMECES2 That students know how to apply their knowledge to their work or vocation in a professional manner and possess the skills that are usually demonstrated through the development and defense of arguments and the resolution of problems within their area of study.
C4 CMECES4 That students can transmit information, ideas, problems and solutions to both a specialised and non-specialised audience

Learning aims
Competences
The student knows, understands, applies and analyzes the design techniques and procedures of axial and radial turbomachines. A17712
A17713
 B958
B960
B961
B5474
B5476
 C1
C2
C4
The student knows, understands and analyzes the performance of turbomachines applied to the study of jet engines actuations. A17712
A17713
 B958
B960
B961
B5474
B5476
 C1
C2
C4

Contents
Topic Sub-topic
Bloque I: BASIC PRINCIPLES AND TURBOMACHINERY ANALYSIS Tema 1: GENERAL CONCEPTS

Tema 2: FUNDAMENTAL THEOREM OF TURBOMACHINERY
Bloque II: TWO-DIMENSIONAL STUDY OF AXIAL TURBINES Tema 1: IMPULSE TURBINES

Tema 2: REACTION TURBINES
Bloque III: TWO-DIMENSIONAL STUDY OF AXIAL COMPRESSORS Tema 1: VELOCITY TRIANGLES

Tema 2: THE STARTING PROBLEM
Bloque IV: TRHEE-DIMENSIONAL STUDY OF AXIAL TURBOMACHINERY Tema 1: RADIAL EQUILIBRIUM

Tema 2: STRESS
Bloque V: RADIAL TURBOMACHINERY Tema 1: RADIAL COMPRESSORS

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
The student will have the support of the teacher to carry out individual or group tutorials. These tutorials can be carried out in person or virtually, but always within the hours established for this purpose.

Assessment
  Description Qualification
Mixed tests It comprises a written test with theoretical and practical questions related to the course’s topics. 70%
It comprises writing a memory and its oral presentation. Its content will be related to the course’s topics. 30%
 
Other comments and second call
(1) The completion of the requested works (individual or group), as well as possible practices activities, will be mandatory to obtain the final grade.
(2) The final grade, weighted between the practical activities and the mixed tests, may be subject to obtaining a minimum grade in each of the parts.
(3) In the second call, the score related to the work carried out during the course will be kept.

Sources of information
Access to Recommended Bibliography in the Catalog ULE

Basic AIAA, AIAA Journal of propulsion and power, AIAA Education Series,
Mattingly, J.D., Aircraft Engine Design, AIAA Education Series,
Hill, Petterson, Mechanics and Thermodinamic of Propulsion, Addison Wesley,
R. I. Lewis, Turbomachinery performance analysis, Arnold, 1996

Complementary Oates, G. C., Aerothermodynamics of Aircraft Engine Components, AIAA Education Series,


Recommendations


Subjects that it is recommended to have taken before
AEROSPACE TECHNOLOGY / 00710312
APPLIED THERMODYNAMICS / 00710315
AERODYNAMICS / 00710318
PROPULSIÓN / 00710320
JET ENGINES / 00710333