TABLE 2A.
Computed drag for various values of viscosity, compared with Batchelor's; their computed ratio appears in the third column
| Viscosity | Computed drag | Drag | Ratio | Computed lift |
|---|---|---|---|---|
| 50 | 134.3 | 120.3 | 1.11 | 0.018 |
| 75 | 184.8 | 176.5 | 1.10 | 0.011 |
| 80 | 185.8 | 176.7 | 1.05 | 0.011 |
| 90 | 187.6 | 194.7 | 0.96 | 0.011 |
| 100 | 233.0 | 215.5 | 1.09 | 0.007 |
The last column contains the computed lift, which should be compared with exact lift—zero.