P1.8.7.1 Measurement of Airfoils in a Wind Tunnel
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Measurement of airfoils in a wind tunnel
In the experiment P1.8.7.1, the air resistance fW and the lift FA of an airfoil are measured as a function of the angle of attack α of the airfoil against the direction of flow. In a polar diagram, FW is graphed as a function of FA with the angle of attack α as the parameter. From this polar diagram, we can read e. g. the optimum angle of attack.
COMPONENTS OF EQUIPMENT SETS:
| 1 | 373 12 | Wind tunnel |
| 1 | 373 041 | Suction and pressure fan |
| 1 | 373 075 | Measurement trolley for wind tunnel |
| 1 | 373 08 | Aerodynamics accessories 2 |
| 1 | 373 14 | Sector dynamometer, 0.65 N |
EXPERIMENT INSTRUCTIONS PLEASE CLICK HERE
