Wcl. Shih et al., EXPERIMENTS ON FLOW PAST ROUGH CIRCULAR-CYLINDERS AT LARGE REYNOLDS-NUMBERS, Journal of wind engineering and industrial aerodynamics, 49(1-3), 1993, pp. 351-368
Data have been obtained in the 12-foot pressurized wind tunnel at NASA
Ames Research Center on flow past smooth and rough circular cylinders
at high Reynolds numbers. Steady and unsteady surface pressures were
measured around and along the cylinders. Analysis of the results provi
des lift and drag coefficients and Strouhal numbers for cylinders of s
everal roughnesses at Reynolds numbers up to 8 x 10(6).