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Educational guide | |||||||||||||||||||||||||||||||||||||||
IDENTIFYING DATA | 2024_25 | |||||||||||||||||||||||||||||||||||||||
Subject | STRUCTURAL AND AEROLASTIC AIRCRAFT DESIGN. | Code | 00713002 | |||||||||||||||||||||||||||||||||||||
Study programme |
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Descriptors | Credit. | Type | Year | Period | ||||||||||||||||||||||||||||||||||||
4.5 | Compulsory | First | First |
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Language |
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Prerequisites | ||||||||||||||||||||||||||||||||||||||||
Department | TECN.MINERA,TOPOGRAF. Y ESTRUC |
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Coordinador |
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iubem@unileon.es jvale@unileon.es vgutp@unileon.es |
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Lecturers |
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Web | http:// | |||||||||||||||||||||||||||||||||||||||
General description | ||||||||||||||||||||||||||||||||||||||||
Tribunales de Revisión |
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Competencies |
Type A | Code | Competences Specific |
A13176 | ||
A13178 | ||
A13181 | ||
A13183 | ||
A13187 | ||
A13189 | ||
A13223 | ||
Type B | Code | Competences Transversal |
B3048 | ||
B3049 | ||
B3050 | ||
B3051 | ||
B3052 | ||
B3053 | ||
B3058 | ||
B3062 | ||
Type C | Code | Competences Nuclear |
C1 | ||
C2 |
Learning aims |
Competences | |||
Analysis and design of aircraft structures | A13181 A13183 A13187 A13189 |
B3048 B3049 B3050 B3051 B3052 B3053 B3062 |
C1 |
Applied aeroelasticity | A13223 |
B3048 B3049 B3050 B3051 B3052 B3053 B3058 |
C1 |
Understand and apply simple fracture mechanics concepts. | A13176 A13178 |
B3050 B3051 |
C1 C2 |
Contents |
Topic | Sub-topic |
BLOCK I. Spacecraft Structures | Topic 1.- One-dimensional structures Topic 2.- Two-dimensional structures |
BLOCK II. Structural instabilities | Topic 3.- Introduction to stability theory Topic 4.- Global buckling Topic 5.- Stability of aircraft skin panels |
BLOCK III. Fatigue and fracture mechanics | Topic 6: Introduction to Fatigue 6.1.- Fatigue Failure Mechanisms 6.2.- Fatigue Failure Models Topic 7: Fatigue Resistance 7.1.- Calculation of Fatigue Stresses 7.2.- Theoretical Fatigue Strength 7.3.- Fatigue Resistance Limit 7.4.- Corrected Fatigue Resistance |
Planning |
Methodologies :: Tests | |||||||||
Class hours | Hours outside the classroom | Total hours | |||||||
Problem solving, classroom exercises | 16 | 24 | 40 | ||||||
Tutorship of group | 1 | 1.5 | 2.5 | ||||||
Lecture | 24 | 36 | 60 | ||||||
Mixed tests | 4 | 6 | 10 | ||||||
(*)The information in the planning table is for guidance only and does not take into account the heterogeneity of the students. |
Methodologies |
Description | |
Problem solving, classroom exercises | The professor will guide students in applying theoretical concepts and results to problem solving, encouraging critical thinking at all times. Exercises will be proposed and students will solve them, thus acquiring skills in using the necessary tools for problem solving. |
Tutorship of group | To guide the student in his learning so that he becomes an autonomous, competent and critical learner in his workplace. |
Lecture | Theoretical classes in which the theoretical foundations of the subject are exposed, reasoned and deduced. At the end of each section, simple exercises will be solved to clarify the theory explained. |
Personalized attention |
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Assessment |
Description | Qualification | ||
Mixed tests | 1.- 80% 2.- 20% |
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Other comments and second call | |||
It will be mandatory to obtain a score of 5 out of 10 in each of the tests. In the second call, the results of the tests taken throughout the semester will be valid, although it is not obligatory to have taken them. In the case of non-participation in the tests, the grade of the final exam will be 100% of the evaluation. English Friendly |
Sources of information |
Access to Recommended Bibliography in the Catalog ULE |
Basic | |
1.- Lakshmi, G, Aircraft Structures, BS Publications, India, 2011 2.- Megson, T. H. G. (Thomas Henry Gordon), Aircraft structures for engineering students / T.H.G. Megson., 2nd ed., New York : Halsted Press, 1990 3.- Arana, J.L., González, J.J., Mecánica de la fractura, Servicio Editorial Universidad del País Vasco, 2002 4.- R.M. Rivello. “Theory and Analysis of Flight Structures”. Mc Graw-Hill. 5.- E.F. Bruhn. “Analysis & Design of Flight Vehicle Structures”. S.R. Jacobs & Associates, Inc. 6.- Martínez, C., Estructuras Aeronáuticas (Problemas resueltos), ETSIA Servicio de publicaciones, Madrid 1998 |
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Complementary | |
Recommendations |