Aerospace Materials I

To understand the structure, composition, processing, properties and performance of different families of metallic materials used in aerospace and the relationship among them. To be able to select metallic materials for applications in different aerospace engineering fields. To know the more adequate standardized tests to evaluate properties and performance of metallic materials, and to analyze the results. Regarding general capabilities or skills, during the year, students will acquire the following abilities: - Ability to solve complex problems. - Ability to look for, to understand and to differentiate the relevant information to be able to take a decision. - Ability to use multi-disciplinary knowledge to solve a problem. - Ability to work in groups and distribute work to face up to complex problems.

CB2: Students are able to apply their knowledge to their work or vocation in a professional manner and possess the competences usually demonstrated through the development and defence of arguments and problem solving within their field of study. CB5: Students will have developed the learning skills necessary to undertake further study with a high degree of autonomy. CG5: Ability to carry out projection activities, technical management, expert appraisal, drafting of reports, opinions, and technical advice in tasks related to Aeronautical Technical Engineering, the exercise of genuinely aerospace technical functions and positions. CG7: Ability to analyse and assess the social and environmental impact of technical solutions. CG9: Ability to analyse and solve aerospace problems in new or unknown environments, within broad and complex contexts, integrated in multidisciplinary and international work teams. CG10: Ability to use computational and experimental tools for the analysis and quantification of engineering problems. CE.CRA5: Understand the technological performance, the techniques for optimising materials and the modification of their properties through treatments. CE.CRA12: Adequate knowledge and application to engineering of: The fundamentals of fluid mechanics; the basic principles of flight control and automation; the main physical and mechanical characteristics and properties of materials. CE.CRA13: Applied knowledge of: the science and technology of materials; mechanics and thermodynamics; fluid mechanics; aerodynamics and flight mechanics; navigation and air traffic systems; aerospace technology; theory of structures; air transport; economics and production; projects; environmental impact. RA1: Have basic knowledge and understanding of mathematics, basic sciences, and engineering within the aerospace field, including: behaviour of structures; thermodynamic cycles and fluid mechanics; the air navigation system, air traffic, and coordination with other means of transport; aerodynamic forces; flight dynamics; materials for aerospace use; manufacturing processes; airport infrastructures and buildings. In addition to a specific knowledge and understanding of the specific aircraft and aero-engine technologies in each of the subjects included in this degree. RA2: Be able to identify aerospace engineering problems, recognise specifications, collect and interpret data and information, establish different resolution methods and select the most appropriate among the available alternatives. RA3: Be able to carry out designs in the field of aerospace vehicles, propulsion systems, navigation and air traffic control, airport infrastructures, or equipment and materials for aerospace use, which comply with the required specifications, collaborating with other engineers and graduates. RA4: Graduates will be able to carry out initial research methods approaches commensurate with their level of knowledge involving literature searches, design and execution of experiments, data interpretation, selection of the best proposal and computer simulation. RA6: Have the necessary skills for the practice of engineering in today's society.

- Solidification of Metals. Generation of the Microstructure. Metal Casting Processes. Cast Structures Defects in Castings. - Metal forming processes. Work hardening. Recovery, Recrystallization and Grain Growth. Effect of metal forming processes on properties and microstructure. Formability. -Phase Diagrams. Invariant Reactions. Influence of alloying elements. Equilibrium phase transformation. - Non-equilibrium phase transformations. TTT diagrams: ITT and CCT. Heat Treatments: Quenching, Tempering, Annealing, Normalizing. Hardenability -Introduction to Fracture. Types of Fracture. Fracture modes. Fracture mechanics. Stress concentration. Griffiths theory. Stress intensity factor. Fracture toughness and Impact test. Brittle Ductile transition. - Introduction to Fatigue. High cycle fatigue. Low cycle fatigue. Effect of variable cycles. Fatigue crack growth.Structural features of fatigue. Designing against fatigue failure -Creep. Creep curve. Effect of stress and temperature on creep. Creep stages. Creep design and life prediction. Developing creep-resistant materials. - Corrosion. Basic electrochemical corrosion. Types of corrosion. Corrosion control and prevention. High temperature corrosion. - Friction. Wear. Friction and wear tests. Lubricants. Wear and friction in metal-working processes. Materials selection for tribological system. - Designation of Aluminium Alloys. Heat treatable aluminium alloys. Non heat treatable aluminium alloy. Applications of Al alloys in aerospace. Mg alloys. - Designation of Titanium alloys. Properties of Ti alloys. Heat Treatments for Ti alloys. Applications. - Ultra high strength steels. PH stainless steels. Maraging Steels. - Ni-based alloys and superalloys. Properties and applications. - Intermetallics in aerospace. Properties and applications. - Main surface treatments: Galvanizing; Electrodepostion; Organic Coatings; CVD; PVD: Thermal Spraying. Thermochemical Treatments. Thermal Barrier Coatings. - Introduction to joining processes. Welding. Welding processes for aerospace applications. - Common NDT method. Visual Inspection. Liquid Penetrants. Magnetic Particle. Eddy Current. Radiographic. Ultrasonic Acoustic Emissions. Method comparison.

-The course will consist of Master Classes where the theory of the topics will be presented and Tutorial Classes where applications and examples will be emphasized and problems exercises will be solved - There will be tutorial sessions for the students - There will be 6 hours of practical laboratory work of compulsory assistance. The laboratory sessions will result in the acquisition of practical abilities related to the content of the course - All the teaching material (lecture notes, handouts, exercises and problems, laboratory manual and additional material) will be distributed to the students through aula global