Aerodynamics Research Laboratory

 | Post date: 2019/11/25 | 
Established in 1990 the Experimental Aerodynamics laboratory initiated its activities in two sections: Student Learning and Industrial Researches. The laboratory has undergone the installation of a subsonic wind tunnel having a 1200*457*457 millimeters test section and wind speed of 45 m/sec. Additional apparatus include balance system for Aerodynamic Force Determination, a 36-branch manometer, a 2-branch manometer, different test models, a CTA machine to measure the flow velocity profile, turbulence and boundary layer thickness which has been employed in both aforementioned sections. Also, a supersonic tunnel is dedicated to the Student Learning Section to support Gas Dynamics studies.

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