2021
DOI: 10.1016/j.csite.2021.101357
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Flow dynamics over a heated cylinder subjected to high temperature ratios

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Cited by 10 publications
(5 citation statements)
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“…fig.10, shows important differences. In particular, the maximum value of C l decreases for the case with r θ = 2, in agreement with the findings by Homsi et al[24].…”
supporting
confidence: 92%
“…fig.10, shows important differences. In particular, the maximum value of C l decreases for the case with r θ = 2, in agreement with the findings by Homsi et al[24].…”
supporting
confidence: 92%
“…Shi et al [44] showed that for a given free-stream Reynolds number, the cylinder heating has no influence on the average drag coefficient and that the latter remains almost constant for free-stream Reynolds numbers between 100 and 200. Hence, the results of Homsi et al [48], obtained for a flow past a cylinder heated at T * w = 1.66 at Re ∞ = 150, as well as the results of Lima E Silva et al [49] for an unheated cylinder at Re ∞ = 150, can be considered here for C d comparisons. Table 4 shows a well agreement between the present drag coefficients and the results of the mentioned above authors [48,49].…”
Section: Case 2: Unsteady Flow Past a Circular Cylindermentioning
confidence: 95%
“…Hence, the results of Homsi et al [48], obtained for a flow past a cylinder heated at T * w = 1.66 at Re ∞ = 150, as well as the results of Lima E Silva et al [49] for an unheated cylinder at Re ∞ = 150, can be considered here for C d comparisons. Table 4 shows a well agreement between the present drag coefficients and the results of the mentioned above authors [48,49]. The Strouhal number obtained for both methods shows an excellent agreement with the results of Shi et al [44].…”
Section: Case 2: Unsteady Flow Past a Circular Cylindermentioning
confidence: 95%
“…This implies that the outer spirals take the bulk temperature of the combustion chamber at any time; we have from the thermocouple, T ( t ) = T ( t ) at some t . For any setup that lacks similar conditions, equations (1)–(3) will have to be solved [11, 12].…”
Section: Mathematical Formulationmentioning
confidence: 99%
“…then T ∞ = T , T is the temperature at the wall. This implies that the outer spirals take the bulk temperature of the combustion chamber at any time; we have from the thermocouple, T (t) = T ∞ (t) at some t. For any setup that lacks similar conditions, equations ( 1)-( 3) will have to be solved [11,12]. Consider the whole material as a finite hollow cylinder of fixed radius r, the inward heat flow can be described by:…”
Section: ∂(ρE)mentioning
confidence: 99%