TABLE III.
Measured and predicted boundary layer properties for stationary airfoil at 0° angle of attack at Rec = 147 814.
| δ*, mm | Θ, mm | H | |
|---|---|---|---|
| Measured | 1 | 0.6 | 2 |
| XFOIL | 0.7 | 0.4 | 1.8 |
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