Research Article

Wake Measurements behind an Oscillating Airfoil in Dynamic Stall Conditions

Table 1

Pressure taps location on the NACA 23012 model midspan section.

Tap numberLocation x/c

10
20.01
30.044
40.096
50.164
60.28
70.358
80.453
90.618
100.76
110.9
120.9
130.767
140.628
150.459
160.373
170.285
180.185
190.118
200.06
210.02