Dr. Stephen Tullis

Forces and moments associated with flow around airfoils and bodies. Finite wings. Potential flow and introduction to panel methods. Thin airfoil theory and symmetric and cambered airfoils. Introduction to aircraft stability and aeroelasticity.
Three lectures; second term
Prerequisite(s): MECHENG 3O04:
3 unit(s)

Compressible flows: Fanno and Rayleigh flows, normal and oblique shocks. Turbomachines: axial and radial flow gas and steam turbines, axial and radial flow compressors and fans.

Three lectures; first term
Prerequisite: MECH ENG 2W04, 3O04

3 unit(s)
Forces and moments associated with flow around airfoils and bodies. Finite wings. Potential flow and introduction to panel methods. Thin airfoil theory and symmetric and cambered airfoils. Introduction to aircraft stability and aeroelasticity.
Three lectures; second term
Prerequisite(s): MECHENG 3O04:

Compressible flows: Fanno and Rayleigh flows, normal and oblique shocks. Turbomachines: axial and radial flow gas and steam turbines, axial and radial flow compressors and fans.

Three lectures (Term 1)

The course introduces the phenomenological features in turbulent flows and the methods used to analyze these flows. This will include developing the Reynolds average equations, investigating the vortex dynamics in these flows, applying the governing equations to different flows and other topics. The course will cover material related to both wall-bounded and freeshear flows.

(Term 2)