Swirling flow effectiveness on controlling the bulk mold flow has been acknowledged recently, concerning the productivity of continuous casting process and its quality. From the practical viewpoint, relationship between the throughput and bulk mold flow is investigated. Following results are obtained:1) Numerical analysis fairly coincide with the experimental results for the cases: nozzle outlet, surface flow and velocity distributions along the narrow face. 2) Surface velocity decreases with increasing the axial length of the nozzle outlet, particularly in length from 20 to 60 mm. 3) For the high throughput case, considerable stable bulk mold flow can be obtained.
Results and ConsiderationIt has been acknowledged that turbulence-k-e model is not appropriate for swirling flow phenomena. However, in my several studies using a water model, the calculated results using the k-e model have fairly coincided with the water-model-experiment-results as shown for several turbulent-flow-cases, within swirl-number (mean tangential velocity across the tube/mean axial velocity across the tube) of 1, even with the considerably high tangential velocity of 2 m/s in the tube. 6,7) On the other case, the calculated results using the k-e model have not coincided with the experimental results, for the case (ϭswirl numberϾ Ͼ1).
12)Namely, in the flow area within the swirl number less than 1, calculation using the k-e model is considered to be effective. Accordingly, in this study, following governing equations were used because almost applied swirl numbers are within 1. Continuity, momentum equations and Realizable k-e model are adopted at the following calculations using the FLUENT-code.13) Where the coefficients C 1 , C 2 , s k , s e , are empirical constants which have the following values C 1 ϭ1.44, C 2 ϭ1.9, s k ϭ1.0, s e ϭ1.2. Boundary conditions: wall function at solid wall; k and e are those derived from the assumption of an equilibrium boundary layer; uniform axial component velocity and radial profiles of tangential velocity described later are assumed, at the nozzle inlet; a constant pressure is assumed at exit boundary; no shear stress is assumed at the free surface; small grid spacing was employed near the domain. In order to ensure the numerical accuracy of the results, the mass and momentum equations are required to be satisfied to within 0.1% of the integrated flow of the quantity through the domain.The radial profiles of the tangential velocity at 20 mm ISIJ International, Vol. 41 (2001) downwards from the nozzle entrance, which are used in calculation, are shown in Fig. 3. Where, W is defined as a mean tangential velocity across the nozzles which correspond to radial profile of tangential velocity shown. Velocity distributions at the outlet of the nozzle for the cases without and with swirl are shown in Fig. 4. For the case without swirl, the flow goes through down and impinges on the well of bottom and rises as a reverse flow. A boundary separation between the flow and curved wall is observed at the upper par...