1985
DOI: 10.1016/0167-6105(85)90040-6
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Aerodynamic forces on structures of circular cross-section. Part 1. Model-scale data obtained under two-dimensional conditions in low-turbulence streams

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Cited by 42 publications
(11 citation statements)
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“…Recently, Hsu et al (2019) performed an experimental work with 38 fabric samples tested on a circular cylinder in a wind tunnel experiment, and concluded that the roughness of the textile materials could be expressed in terms of the Nikuradse's sand-grain roughness (Nikuradse, 1937). By this finding, the effect of textile roughness on the drag crisis phenomenon could be described by the empirical relations originally proposed for other types of roughness elements (Basu, 1985). As for the drag crisis phenomenon of flow over a circular cylinder, a significant number of works can be found in the literature (Achenbach, 1968;Bearman, 1969;Farell & Blessman, 1983;Roshko, 1993;Schewe, 1983;Wieselsberger, 1922;Zdravkovich, 1997).…”
Section: Introductionmentioning
confidence: 79%
“…Recently, Hsu et al (2019) performed an experimental work with 38 fabric samples tested on a circular cylinder in a wind tunnel experiment, and concluded that the roughness of the textile materials could be expressed in terms of the Nikuradse's sand-grain roughness (Nikuradse, 1937). By this finding, the effect of textile roughness on the drag crisis phenomenon could be described by the empirical relations originally proposed for other types of roughness elements (Basu, 1985). As for the drag crisis phenomenon of flow over a circular cylinder, a significant number of works can be found in the literature (Achenbach, 1968;Bearman, 1969;Farell & Blessman, 1983;Roshko, 1993;Schewe, 1983;Wieselsberger, 1922;Zdravkovich, 1997).…”
Section: Introductionmentioning
confidence: 79%
“…Almost always based on wind tunnel results, available forecasting models of these quantities are referred to very standard situations. Concerning circular cylinders, a large amount of well-established data exist related to the drag coefficient and Strouhal number (Basu, 1985); data become highly scattered when related to the lift coefficient. On the contrary, measures concerning non-circular shapes are scarce as the variability of possible configurations increases.…”
Section: Wind-excited Response and Parametersmentioning
confidence: 99%
“…In low-turbulence streams, the flow field undergoes some dramatic changes, and three regimes can be identified: sub-critical for 1500(Re(2;10, super-critical for Re'2;10, and post-critical for Re'10. The nature of the transition from sub-critical to super-critical, and the transition from supercritical to post-critical, has been discussed by Basu (1985). For the range of Re from about 10 to at least 2;10, where the point of transition is close to the point of separation and the major portion of the free shear layer is turbulent, the flow field is nearly independent of Re.…”
Section: Introductionmentioning
confidence: 96%