1975
DOI: 10.1007/bf01681556
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Investigation of the flow around transverse cylinders

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Cited by 87 publications
(25 citation statements)
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“…The free stream Mach number in both cases was set to 0.3. The streamlines for the flow at 20 are shown in Figure 6 whereas Table 1 lists the separation length and angle and the drag coefficient in comparison with reference values from literature [14,15]. The agreement is quite satisfactory, only the separation angle is predicted too low, which might be due to the lack of considering the pressure gradient in the wall-layer.…”
Section: Laminar Flow Past a Circular Cylindermentioning
confidence: 51%
“…The free stream Mach number in both cases was set to 0.3. The streamlines for the flow at 20 are shown in Figure 6 whereas Table 1 lists the separation length and angle and the drag coefficient in comparison with reference values from literature [14,15]. The agreement is quite satisfactory, only the separation angle is predicted too low, which might be due to the lack of considering the pressure gradient in the wall-layer.…”
Section: Laminar Flow Past a Circular Cylindermentioning
confidence: 51%
“…Its settling y-velocity approaches a constant value, which is the particle terminal velocity caused by the balance of gravitational and viscous forces. The viscous force is calculated using an empirical correlation provided by Sucker and Brauer [16] for a drag coe cient in a ow past a cylinder of unit length …”
Section: Resultsmentioning
confidence: 99%
“…A comprehensive comparison of the drag coefficients obtained from this IFEM study and numerical experimental solution of others [13,17,18,31,[39][40][41][42] at different Reynolds numbers is presented in Table 1 and Fig. 6.…”
Section: Drag and Lift Coefficientsmentioning
confidence: 99%