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Educational guide | |||||||||||||||||||||||||||||||||||||||
IDENTIFYING DATA | 2024_25 | |||||||||||||||||||||||||||||||||||||||
Subject | AEROELASTICITY IN PROPULSIVE SYSTEMS | Code | 00710331 | |||||||||||||||||||||||||||||||||||||
Study programme |
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Descriptors | Credit. | Type | Year | Period | ||||||||||||||||||||||||||||||||||||
6 | Compulsory | Third | Second |
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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 gbalg@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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Competencias |
Code | |
A17705 | |
B958 | |
B5474 | |
B5475 | |
B5477 | |
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. |
C3 | CMECES3 That students have the ability to gather and interpret relevant data (normally within their area of study) to make judgments that include reflection on relevant issues of a social, scientific or ethical nature. |
C5 | CMECES5 That students have developed those learning skills necessary to undertake further studies with a high degree of autonomy |
Learning aims |
Competences | |||
That students have the ability to gather and interpret relevant data (usually within their field of study) in order to make judgments that include reflection on relevant social, scientific, or ethical issues. | B5474 B5475 |
C3 |
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Appropriate and applied knowledge of fracture mechanics of continuous media and dynamic, fatigue, structural instability, and aeroelasticity approaches to engineering. | A17705 |
B958 |
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The ability to analyze, synthesize, solve problems, and make decisions. | B5474 |
C2 |
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Ability to learn independently and individually in any field of engineering. | B5477 |
C5 |
Contents |
Topic | Sub-topic |
BLOCK I: STRUCTURAL DYNAMICS | Topic 1: Introduction. Topic 2: Systems of one degree of freedom. Topic 3: Systems of N degrees of freedom. Topic 4: Continuous systems. |
BLOCK II: AEROELASTICITY | Topic 5: Static aeroelasticity of the airfoil. 5.1.- Two-dimensional divergence. 5.2.- Two-dimensional aileron reversal. Topic 6: Dynamic aeroelasticity of the airfoil. 6.1.- Flutter. 6.2.- Theory of the oscillating airfoil in an incompressible flow. 6.3.- Theory of the airfoil in a supersonic flow. 6.4. Dynamic response to discrete gusts and atmospheric turbulence. Topic 7: Aeroelasticity of turbomachines. 7.1.- Buffet. 7.2.- Separation flutter. 7.3.- Aeroelastic design of engine components. |
Planning |
Methodologies :: Tests | |||||||||
Class hours | Hours outside the classroom | Total hours | |||||||
Problem solving, classroom exercises | 25 | 37.5 | 62.5 | ||||||
Tutorship of group | 2 | 3 | 5 | ||||||
Lecture | 29 | 43.5 | 72.5 | ||||||
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 are solved to clarify the theory explained. |
Personalized attention |
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Assessment |
Description | Qualification | ||
Mixed tests | T1: 80 % T2: 20 % |
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Other comments and second call | |||
The final exam of the course is divided into two parts. One part corresponding to Block 1: Vibrations (40% of the final grade) and another part corresponding to Block 2: Aeroelasticity (60% of the final grade). In order to pass the final exam, it will be necessary to obtain at least 5 out of 10 points in each of the parts that make up the final exam of the subject. In the second call, the results of the tests taken throughout the semester are valid, although it is not obligatory to have taken them. In case of not having done the individual work, 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 | |
Chopra, A.K. (2014): Dinámica de estructuras. Pearson. Clough,R.W. y Penzien, J. (1993): Dynamics of Structures.Mc Graw Hil . de la Fuente Tremps, Enrique (2015): Fundamentos de Dinámica Estructural. Garceta Grupo Editorial. García-Fogeda, P. y Sanz, A. (2013): Introducción a las vibraciones. Garceta Grupo Editorial. Géradin, M. y Rixen, D.J. (2015): Mechanical Vibrations. Wiley. Rao, S.S.(1995): Mechanical Vibrations. Addison-Wesley. VV.AA: (1991): Problemas de Vibraciones en Estructras. C.I.C.Cy P. y ACHE. GARCÍA-FOGEDA, P. Y ARÉVALO, F. "Introducción a la Aeroelasticidad", Editorial Garceta, Septiembre, 2015. LÓPEZ DÍEZ, J. Y GARCÍA- FOGEDA, P. "Problemas de Aeroelasticidad". ETSI Aeronáuticos, UPM. DOWELL, EH., CURTISS, HC., SCANLAU, RH Y F. SISFO. FR. "A Modern Course in Aeroelasticity". Sijthoff and Noordhoff, 1980. BISPLINGHOFF, RL. Y ASHLEY, H. "Principles of Aeroelasticity". Dover, 1962. BISPLINGHOFF, RL, ASHLEY H., Y R.L. HALFMAN. RL. "Aeroelasticity". Ed. Addison-Wesley, 1955. FUNG. YC. "An Introduction to the theory of Aeroelasticity". Wiley, 1955. WRIGHT, JAN R. Y COOPER, JONATHAN E. "Introduction to aircraft aeroelasticity and loads".American Institute of aeronautics and Astronautics; Chichester Reston, Virginia, 2007. |
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Complementary | |
Recommendations |
Subjects that it is recommended to have taken before | ||||||
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