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Turbomachinery Theory and Design

Code 18172
Year 2
Semester S1
ECTS Credits 6
Workload PL(15H)/T(30H)/TP(15H)
Scientific area MECÂNICA COMPUTACIONAL
Entry requirements N.A.
Learning outcomes The primary objectives of this course are: 1. To provide a thorough understanding of the principles governing turbomachinery. 2. To enable students to analyze and design pumps, turbines, compressors, and fans. 3. To develop computational skills for simulating turbomachinery performance using software like ANSYS Fluent, BladeGen, TurboGrid, and CFX. 4. To introduce experimental techniques for performance evaluation and validation. 5. To link theoretical knowledge with real-world applications in energy and aerospace sectors. 6. To give students a complete design-analysis-evaluation workflow by integrating theory, simulation, and experiments.
Syllabus 1. Basic definitions and components. 2. Turbomachinery Fluid Mechanics 3. Axial turbomachines: Cascade geometry and analysis forces, Velocity triangles, Turbine stage design parameters, Velocity diagrams of the compressor stage, Compressor losses, Preliminary compressor/turbine stage design, Multistage compressor and Off-design performance 4.Dimensional Analysis: Buckingham theorem, and Performance Characteristics, Specific speed and specific diameter and Cordier diagram 5. Radial turbomachines: Principle components and Impeller shape, Thermodynamic analysis and velocity triangles, performance curve and slip factors 6.Computational Fluid Dynamics (CFD): Geometry creation of rotor and stator for an axial turbomachine. Mesh generation for the rotor and stator passage of an axial flow machine, CFD simulation of Axial turbomachine, post processing of data 7.Experimental Analysis: performance evaluation of a centrifugal ventilator.
Main Bibliography -José Carlos Páscoa Marques (2017), Turbomáquinas – Uma Abordagem Moderna, PUBLINDÚSTRIA. -Dixon, S. L., & Hall, C. A. (2014). Fluid Mechanics and Thermodynamics of Turbomachinery. Butterworth-Heinemann. -Yahya, S. M. (2017). Turbines, Compressors and Fans. Tata McGraw Hill. -Lakshminarayana, B. (1996). Fluid Dynamics and Heat Transfer of Turbomachinery. Wiley.
Teaching Methodologies and Assessment Criteria The assessment is based on: 1.Project Work (40%) 2.Written Exam (40%): 3. Homework Assignments (10%) 4. Laboratory work (10%): Students must obtain 10/20 for each of the above component to pass the course (in other words, deserving the homework and project is obligatory)
Language Portuguese. Tutorial support is available in English.
Last updated on: 2026-02-09

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