Study Programmes 2016-2017
| AERO0015-1 | ||||||||
| Mechanical design of turbomachinery | ||||||||
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Duration :
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| 30h Th, 30h Pr, 30h Proj. | ||||||||
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Number of credits :
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Lecturer :
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| Jean-Claude Golinval | ||||||||
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Language(s) of instruction :
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| English language | ||||||||
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Organisation and examination :
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| Teaching in the first semester, review in January | ||||||||
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Units courses prerequisite and corequisite :
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| Prerequisite or corequisite units are presented within each program | ||||||||
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Learning unit contents :
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| Turbomachinery Rotordynamics : Types of Modelling, Computation of Forward and Backward Critical Speeds, Campbell Diagram, Stability Analysis, Harmonic and Transient Responses, Multi-rotor behavior, Design of bearings, Instability Phenomena. Dynamics of Blades and Disks : Campbell Diagram, External Excitation Sources, Aeroelastic Problems, Bird Impact. Static Analysis of Compressor Blades : Leaning, Effect of Pre-Twist, Bending/Torsion Coupling. Static Analysis of Disks : Design Criteria. Lifetime Calculations of Turbine Blades. | ||||||||
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Learning outcomes of the learning unit :
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| The objective is to present the methods used in the aeronautical industry to analyze the dynamical behavior of turbomachines and to design mechanical components of turbojet engines such as compressor and turbine blades and disks. | ||||||||
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Prerequisite knowledge and skills :
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| This course requires basic knowledge in structural dynamics and of the finite element method. | ||||||||
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Planned learning activities and teaching methods :
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| Projects will be assigned to the students. It will give hands-on practice with methods used for the mechanical design of turbomachines. | ||||||||
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Mode of delivery (face-to-face ; distance-learning) :
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| The course is organised face-to-face during the 1st quadrimester. | ||||||||
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Recommended or required readings :
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Assessment methods and criteria :
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| The final grade will be based on the project report and a written exam:
1. Students will be assigned a project. The grade will be based on the results and the quality of the report (scientific and technical content, conciseness, structuring of the written report and clarity of the text). 2. The written exam will consist in answering to questions on the course materials. A special attention will be devoted to the knowledge and to the understanding of the theoretical concepts. No document is allowed for the examination. The final assessment is based on the weighted geometric average of the project reports and the written exam. The final note is calculated as follows: Final note = (Project)^(0.5) * (Exam)^(0.5) |
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Work placement(s) :
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Organizational remarks :
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Contacts :
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| Jean-Claude Golinval (JC.Golinval@ulg.ac.be) | ||||||||
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Items online :
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 | AERO0015 - Mechanical Design of Turbomachinery Copy of the slides. |
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