Credits: 1
- Introduction into the wind tunnel systems, applications and aerodynamic measurements
- Total and static pressure measurements of the wind tunnel test section by pitot tube
- Flow visualization of the 2D airfoil by smoke generator in order to investigate the initial angle of attack and velocity effects, qualitatively
- Pressure distribution measurements over the cylinder (cylinder axis normal to the flow) at different wind tunnel velocity, and estimation of separation points
- Investigation of the roughness effects on drag coefficient of the sphere, cylinder and …
- Aerodynamic load measurements of the airplane model at subsonic speeds in order to investigate the initial angle of attack, yaw angle, roll angle and aircraft stability
- Investigation of the flap angle over the Cp distribution of an airfoil
- Boundary layer investigations of the flat plate by pressure measurements and estimation of the parameters such as displacement thickness, boundary layer profile and …
- Investigation of the Reynolds Number effects at above experimental test
- Surface pressure measurements of the airfoil in order to calculate aerodynamic coefficients
- Hotwire calibration for velocity and turbulent intensity measurements
- Investigations of the different flap configurations on static stall angle and lift increments