الاختبارات الايروديناميكية بالنفق الهوائي

Title	Wind tunnel aerodynamic tests
Trainers	Prof. Dr. Kamal A. AbedDr. Hany E. FawazEng. Amr A. El-Feki
Duration	3 days
Contents	1.      Specifications of open loop wind tunnel with its test section (60x60x120 cm)Variable speed ranges from 0-26 m/s2.      Wind tunnel is instrumented with suitable sensors to measure aerodynamic forces and pressure distribution.3.      Automatic temperature & velocity scanner system complete with software for at least 12 sensors.4.      Ten sets of sensors for velocity and temperature measurements.5.      Air speed indicated on inclined manometer directly calibrated in m/s6.      Contraction area ratio 3:17.      Motor rating 2kW.8.      Operation of the wind tunnel9.      Preparation of the examined models10.  Measurements of the torque, RPM, Pressure, Temperature, Wind speed across the test section using transverse mechanism .11.  Smoke generator and visualization of the flow around the airfoil.12.  Sensors connected to Data Acquistion of national instruments DAQ are ready to be viewed on the software of Labview.13.  Experimental trainee on all the above system

شاركها

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