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Aerodynamics I

Code 10361
Year 3
Semester S1
ECTS Credits 6
Workload TP(60H)
Scientific area Aeronautics and Astronautics
Entry requirements not applicable
Mode of delivery Face to Face.
Work placements None.
Learning outcomes Teaching Block I - Fundamentals of Fluid Mechanics
Objective: To provide an introduction to fluid properties, the application of the basic laws of mechanics and the use of experimental techniques and computational fluid mechanics.
Skills: Ability to analyze real situations of fluid flow, design of systems using concepts of one-dimensional and incompressible flows.
Teaching Block II - Introduction to Aerodynamics
Objective 1. To know and understand the balance of forces in several instances of flight of an aircraft.
Objective 2. Capacity of potential and incompressible flow analysis.
Objective 3. To use concepts incompressible potential flow to the analysis of real flows.
Objective 4. To extend the concepts of incompressible potential flow to a bi-dimensional situation.
Objective 5. To use the concepts of flow incompressible potential for the airfoil project and analysis.
Skills: Ability to analyze and design airfoils using potential flow analysis.
Syllabus Teaching Block I - Fundamentals of Fluid Mechanics
Fundamental concepts. Fluid Statics. Fluid Dynamics: control volume analysis; differential / infinitesimal analysis; dimensional/experimental analysis. Turbomachinery. Introduction to free surface flows.
Teaching Block II - Introduction to Aerodynamics
The balance of forces in several instances of flight of an aircraft, the physical mechanism of lift production. Potential and incompressible flows. Description of the flow field. Conservation of mass; the concept of stream function. Transport of momentum, Navier-Stokes equations. Transport of mechanical energy, Bernoulli equation, the concept of potential velocity. Pressure equation. Integral relations for a control volume. Evaluation of the drag of a two-dimensional body by analysis of the shear layer. Jones method. Effect of the pressure gradient. Separation. Incompressible flow analysis in real situations. Votex Flow. Incompressible potential flow to a bi-dimensional situation.
Main Bibliography Brederode, V. de, Fundamentos de Aerodinâmica Incompressível, IDMEC, IST, Lisboa.
Oliveira, L.A., Lopes, A.G., “Mecânica dos Fluidos”, Lidel – Edições Técnicas, 6ª Ed., 2020, ISBN – 978-989-752-492-9.
Barata, J.M.M., Mecânica dos Fluidos-Trabalhos de Laboratório, Universidade da Beira Interior.
Silva, A.R.R., Slides de Aerodinâmica I com exercícios propostos, Universidade da Beira Interior, 2020.
Massey, B.S., “Mecânica dos Fluidos”, Fundação Calouste Gulbenkian, Serviços de Educação e Bolsas, Lisboa, 2002, ISBN:-972-31-0945-X.
Batchelor, G.K., An Introduction to Fluid Dynamics, Cambridge University Press.
Doebelin, E.O., Measurements Systems – Application and Design, McGraw-Hill Book Co.
Plotkin, A., Katz, J., Low-Speed Aerodynamics-From Wing Theory to Panel Methods, McGraw-Hill Book Co.
Stinton, D., The Design of the Aeroplane, Blackwell Science.
Streeter, V.L., Wylie, E.B., Fluid Mechanics, McGraw-Hill Book Co.
White, F. M. Fluid Mechanics. McGraw-Hill Book Co.
Teaching Methodologies and Assessment Criteria The methodology based on the solution of problems and laboratory tests is the closest to the practical situation where an engineer performs his job.
The assessment of knowledge is based on the final exam (individual).
1) Final Exam (individual)
The final exam (NEF) consists of a written test (NE) and oral exam (NEO). The final exam grade, NEF, is calculated as follows:
- if NE => 16 values and performed the oral exam, then NEF = NEO;
- if NE => 16 values and not performed the oral exam, then NEF = 16 values;
- if 9,5 <= NE < 16 values, then NEF = NE;
- if NE < 9.5 values, then NEF = NE ("Disapproved").
Admission to the final exam depends on the achievement of frequency according to the criteria below.
Language Portuguese. Tutorial support is available in English.
Last updated on: 2024-11-14

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