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CENG 113 Dynamics of Turbomachines (2.4 unités d'EP)

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Nota : Ceci est la version 2017–2018 de l'annuaire électronique. Veuillez mettre à jour l'année dans la barre d'adresse de votre navigateur pour une version plus récente de cette page, ou .

Offered by: Fac Partner & Summer Studies (École d'éducation permanente)

Vue d'ensemble

Génie (CCE) : Aircraft/helicopter engines architecture (compressor, turbine, combustion chamber). General equations of motion in rotordynamics (basic assumptions and parametrization). Shaft (simplifying assumptions and rotating beams), supporting devices (journal and roller bearings). Finite element discretization, structural matrices (mass, stiffness, gyroscopic terms, damping). Modal analysis – eigenfrequencies and modes of vibration, Campbell diagrams, critical rotational velocities. Rotor imbalances, forced responses, frequency domain analysis. Bladed disk assemblies, mistuning and cyclic symmetry.

Terms: This course is not scheduled for the 2017-2018 academic year.

Instructors: There are no professors associated with this course for the 2017-2018 academic year.

  • 15 hours of classroom instruction, 9 hours of additional work (project).

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