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Experiments on flow past rough circular cylinders at large Reynolds numbers
AbstractData 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 provides lift and drag coefficients and Strouhal numbers for cylinders of several roughness at Reynolds numbers up to 8 × 106.
Experiments on flow past rough circular cylinders at large Reynolds numbers
AbstractData 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 provides lift and drag coefficients and Strouhal numbers for cylinders of several roughness at Reynolds numbers up to 8 × 106.
Experiments on flow past rough circular cylinders at large Reynolds numbers
Shih, W.C.L. (Autor:in) / Wang, C. (Autor:in) / Coles, D. (Autor:in) / Roshko, A. (Autor:in)
Journal of Wind Engineering and Industrial Aerodynamics ; 49 ; 351-368
01.01.1993
18 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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