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Computer Aided Aeronautical Design

Code 10355
Year 2
Semester S1
ECTS Credits 6
Workload PL(15H)/TP(45H)
Scientific area Aeronautics and Astronautics
Entry requirements No entry requirements.
Mode of delivery Theory, practice and laboratories.
Work placements Not applicable.
Learning outcomes Introduction to the airplane: uses, types, configurations and nomenclature. To have basic notions about airplane design, development and manufacture and the disciplines involved. Introduction to Computer Aided Engineering (CAE), with special emphasis on Computer Aided Design (CAD), including Computer Aided Analysis (CAA), Computer Aided Manufacturing (CAM) and Computer Numerical Controlled (CNC) manufacture.
Syllabus 1. Introduction to the curricular unit: objectives and program; teaching methodologies and evaluation.
2. Introduction to the airplane: uses, types, configuration and nomenclature.
3. Introduction to CAE: CAD with CATIA V5, CAM/CNC. Introduction to aircraft design disciplines and CAA: aerodynamics, propulsion and performance, stability and control, structures and materials, weight and balance.
4. Introduction to aircraft design: concepts selection and design philosophy. Introduction to optimization in aircraft design.
Main Bibliography Silvestre M. A. R., Introduction to Aircraft Development. Lecture Notes 2022
Barnard, R. H., & Philpott, D. R. (2010). Aircraft flight: a description of the physical principles of aircraft flight. Pearson Education.
Anderson, J. D. (1989) Introduction to Flight, McGraw-Hill.
S.F. Hoerner, "Fluid dynamic drag", Self published, Midland Park, New Jersey.
Cutler, J. (1999), Understanding Aircraft Structures, Third Edition, Blackwell Science;
Relvas, C. (2002), Controlo Numérico Computorizado, Publindústria.
Zeid, I. (1991). CAD/CAM theory and practice. McGraw-Hill Higher Education.
Mattson, M. (2009). CNC programming: principles and applications. Cengage Learning
Teaching Methodologies and Assessment Criteria During the teaching-learning assessment period, the written attendance test is worth 40% of the grade and focuses on theoretical-practical subjects. It consists of two parts of equal weight: the first is carried out without consultation or calculator; the second allows the use of a calculator and consultation on paper. The individual assignment is worth 10% of the teaching-learning grade, it is mandatory and consists of a conceptual sketch of the airplane individually designed to meet the regulation of the Challenge/competition of the discipline. The group work consists of the design, construction and testing of an R/C model aircraft with the objective of maximizing a performance function defined in the regulation of the Challenge/competition of the discipline, worth 50%.
Language Portuguese. Tutorial support is available in English.
Last updated on: 2025-01-17

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