Table I.
Comparison of experimental and computational values of lift (CL) and drag (CD) coefficients and Strouhal numbers (St) for flow past a circular cylinder at Re = 200.
| CL | CD | St | |
|---|---|---|---|
| Lai and Peskin [68] | — | — | 0.190 |
| Linnick and Fasel [69] | ±0.69 | 1.34 ± 0.044 | 0.197 |
| Liu et al. [70] | ±0.69 | 1.31 ± 0.049 | 0.192 |
| Taira and Colonius [67] (Case C) | ±0.68 | 1.34 ± 0.047 | 0.195 |
| Roshko (experimental) [70] | — | — | 0.190 |
| Williamson (experimental) [70] | — | — | 0.197 |
| present (four-point kernel, N = 128, Mfac = 2) | ±0.70 | 1.36 ± 0.046 | 0.195 |