CENG 113 Dynamics of Turbomachines (2.4 CE units)

Note: This is the 2016–2017 edition of the eCalendar. Update the year in your browser's URL bar for the most recent version of this page, or click here to jump to the newest eCalendar.

Offered by: Fac Partner & Summer Studies (School of Continuing Studies)


Engineering (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 2016-2017 academic year.

Instructors: There are no professors associated with this course for the 2016-2017 academic year.

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