1976
DOI: 10.1017/s000192590000768x
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A Theoretical Study of Body Drag in Subcritical Axisymmetric Flow

Abstract: SummaryA method of predicting body drag in subcritical axisymmetric flow is outlined which requires only detailed body shape, free-stream conditions and transition point to be prescribed. Results of calculations for a range of body shapes are shown essentially to confirm information in Royal Aeronautical Society Data Sheets but clearly demonstrate that fineness ratio alone is not sufficient to characterise body shape. For example, at a fixed fineness ratio of 0.18, detailed changes in body contour are shown to… Show more

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Cited by 125 publications
(68 citation statements)
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“…Unlike traditional Savonius turbine with semi-circular blades, this modified Savonius turbine has its blade shape generated from the Myring Equation [20]. The blade of a traditional Savonius turbine generates drag during the returning half cycle,  between π and 2π, which limits the efficiency of the turbine.…”
Section: The Modified Savonius Wind Turbine and Parameters Definitionmentioning
confidence: 99%
See 1 more Smart Citation
“…Unlike traditional Savonius turbine with semi-circular blades, this modified Savonius turbine has its blade shape generated from the Myring Equation [20]. The blade of a traditional Savonius turbine generates drag during the returning half cycle,  between π and 2π, which limits the efficiency of the turbine.…”
Section: The Modified Savonius Wind Turbine and Parameters Definitionmentioning
confidence: 99%
“…Tian et al [19] carried out CFD simulations of Savonius with elliptical blades. This paper concerns a Savonius wind turbine that has novel blade shapes developed from the Myring Equation [20]. The effect of the blade fullness on the turbine performance is studied over a range of tip speed ratios.…”
Section: Introductionmentioning
confidence: 99%
“…The lengths of the three sections are 0.2 m, 0.7 m, and 0.4 m, respectively. In order to obtain a low-drag shape, the Myring Equation [17] is used to design the shape of the AUV nose. The Myring Equation is widely used in the design of AUV hulls [10].…”
Section: Geometry Configurationmentioning
confidence: 99%
“…The hull has been designed based on the Myring hull profile equations (Myring, 1976) which are known to produce minimum drag force for a given fineness ratio (l/d), that is, the ratio of its length to its maximum diameter. The shapes of the nose and tail sections are determined from (1) and (2), respectively:…”
Section: Hull Designmentioning
confidence: 99%