This course is designed to integrate classroom activities with laboratory experience in incompressible aerodynamics. It includes the wind tunnel testing of
symmetric and cambered airfoils. Pressure distribution around the airfoil and cylinder is studied for the calculation of lift and drag acting on them. Aircraft
model is used in flight demonstration wind tunnel to demonstrate different phases of flight to the students. Flow visualization is studied with the help of
Smoke tunnel and laminar flow table. The concept of vortex flow is demonstrated with help of hydraulic bench. This course acts as supplement to the
theory course on incompressible aerodynamics.
- Teacher: Muhammad