Aero Lab 1

 | Post date: 2019/11/26 | 
Supervisor: Dr.mohammad.saeedi

Phone:+98(21)64545635
Location: 1st floor, AE Department.


 


Introduction

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


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