MEC 475

About Course:

Course Code: MEC 475

Course Name: AERODYNAMICS

Credit Hour: 3

Inviscid incompressible flow to include potential function, stream function, circulation and basic flows; KuttaJoukowski theorem; aerofoil theory and wing theory.

Drag, aircraft propulsion and propeller; static performance problem; special performance problem. Introduction to stability and control: longitudinal stability and control; lateral and directional stability and control.

Course Outcomes (COs):

1. Study and analysis the inviscid incompressible flow

2. Analysis the drag and propulsion for solving complex static and special performance problem.

3. Study the control and stability theory.

4. Able to utilize the suitable software to analyze the aerodynamic performance

5. Able to write a report and to present it

Targeted Program Outcomes (POs):PO1, PO2, PO5, PO10