1982
DOI: 10.1017/s0022112082002742
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Discrete-vortex simulation of a turbulent separation bubble

Abstract: The discrete-vortex model is applied to simulate the separation bubble over a two- dimensional blunt flat plate with finite thickness and right-angled corners, which is aligned parallel to a uniform approaching stream. This flow situation is chosen because, unlike most previous applications of the model, the separation bubble is supposed to be strongly affected by a nearby solid surface. The major objective of this paper is to examine to what extent the discrete-vortex model is effective for such a flow. A sim… Show more

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Cited by 96 publications
(64 citation statements)
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“…7 and 9 in Chen [41], where x = 1.1, 2.1 and 3.6 cm represent the linear distance from the concave of step to the section respectively. At x = 1.1 and 2.1 cm, the measurements are within the shadow of the step, which is a notoriously difficult location to simulate flow velocity [50]. The simulated velocities are in agreement with the measurements.…”
Section: Verification Of Simulated Velocity Profilessupporting
confidence: 62%
“…7 and 9 in Chen [41], where x = 1.1, 2.1 and 3.6 cm represent the linear distance from the concave of step to the section respectively. At x = 1.1 and 2.1 cm, the measurements are within the shadow of the step, which is a notoriously difficult location to simulate flow velocity [50]. The simulated velocities are in agreement with the measurements.…”
Section: Verification Of Simulated Velocity Profilessupporting
confidence: 62%
“…Previous studies also yielded the relation of the recirculation length varying with Re for squares [10,11] and triangulars [12], as well as the linear relation of vortex shedding frequency, St , varying with 1/2 Re  for squares and triangles [13]. For the inviscid flow past polygonal obstacles, we also found studies for pure potential flow [14] and the vortex flow [15,16].…”
Section: Introductionsupporting
confidence: 56%
“…Once the vector C is determined, the flow velocity can be evaluated at any point. The position of each of the shed vortices is updated according to the second-order scheme (Kiya et al, 1982) x…”
Section: The Velocity Fieldmentioning
confidence: 99%