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 number | Location x/c |
| 1 | 0 | 2 | 0.01 | 3 | 0.044 | 4 | 0.096 | 5 | 0.164 | 6 | 0.28 | 7 | 0.358 | 8 | 0.453 | 9 | 0.618 | 10 | 0.76 | 11 | 0.9 | 12 | 0.9 | 13 | 0.767 | 14 | 0.628 | 15 | 0.459 | 16 | 0.373 | 17 | 0.285 | 18 | 0.185 | 19 | 0.118 | 20 | 0.06 | 21 | 0.02 |
|
|