• 제목/요약/키워드: 다중 충돌제트 냉각

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난류 효과를 포함한 다중 충돌 제트의 냉각 특성에 대한 수치적 연구 (NUMERICAL STUDY ON COOLING CHARACTERISTICS OF MULTIPLE IMPINGING JETS INCLUDING THE EFFECT OF TURBULENCE)

  • 전진호;손기헌
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2009년 춘계학술대회논문집
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    • pp.321-328
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    • 2009
  • Free surface impinging jet on a moving plate, which is applicable to cooling of hot metals in a steel-making process, is investigated numerically by solving the Navier-Stokes equations in the liquid and gas phases. The free surface of liquid-gas interface is tracked by a level-set method which is improved by incorporating the ghost fluid approach based on a sharp-interface representation. The method is further improved by employing a nonequilibrium $\kappa-\varepsilon$ turbulence model including the effect of low Reynolds number. The computations are made to investigate the effects of the nozzle pitch, moving velocity of plate and jet velocity on the interfacial motion and the associated flow and temperature fields.

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핵융합로 디버터 다중충돌제트 냉각시스템의 형상변화가 열수력학적 특성에 미치는 영향 (GEOMETRICAL EFFECTS ON THERMAL-HYDRAULIC PERFORMANCE OF A MULTIPLE JET IMPINGEMENT COOLING SYSTEM IN A DIVERTOR OF NUCLEAR FUSION REACTOR)

  • 정효연;김광용
    • 한국전산유체공학회지
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    • 제22권1호
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    • pp.26-36
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    • 2017
  • A numerical study has been performed to evaluate thermal-hydraulic performance of a finger type cooling module with multiple-jet impingement in a divertor of nuclear fusion reactor. To analyze conjugate heat transfer in both solid and fluid domains, numerical analysis of the flow using three-dimensional Reynolds-averaged Navier-Stokes equations has been performed with shear stress transport turbulence model. The computational domain for the cooling module consisted of a single fluid domain and three solid domains; tile, thimble, and cartridge. The numerical results for the temperature variation on the tile were validated in comparison with experimental data under the same conditions. A parametric study was performed with four geometric parameters, i.e., angles between x-axis and centerlines of hole 1, 2, 3 and 4. The results indicate that the heat transfer rate was increased by 2.7% and 0.7% by the angle ${\theta}_1$ and angle ${\theta}_2$, respectively, and that the pressure drop was decreased by up to 1.8% by the angle ${\theta}_3$.