Spring 2012

 Laboratory #1: Force Measurements in a Subsonic Wind Tunnel

A data report only is required for this laboratory. Please carefully follow the instructions for data report formats.



Additional Instructions
After the airfoil (2-d) data listed in the lab manual are acquired, but before you go on to the wing (3-d) measurements, do the following. Acquire another set of lift and drag measurements for the last flap deflection angle, but for a wind speed roughly 60-70% of the value you used originally. Make the measurements at the same angles of attack used in the original data. Treat this data in the Results section as you would all the other data acquired in the lab.


 

Questions
Your report must also include answers to the following questions in the appropriate section.


 

  1. Compare the lift curve slope that you measured for the airfoil with that predicted by thin airfoil theory, including effects of camber.  Be sure to include in your discussion the results obtained at the lower air speed.  Also comment on any observed differences between the behavior of the drag coefficient versus angle of attack for the airfoil versus the wing.
  2. Discuss the effect of Reynolds number on the stall angle.
  3. Discuss the reasons for the difference in stall angle measurements with and without the end plates.