• Title/Summary/Keyword: Unstructured Fixed-Grid System

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Numerical Analysis on Flow and Heat Transfer in Twin-Roll Strip Casting Using an Unstructured Fixed-Grid System (비정렬 고정격자계를 이용한 쌍롤 박판주조에서의 유동장 및 열전달 해석)

  • Lee, Jun-Sik;Lee, Ju-Myeong;Jeong, Jae-Dong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.26 no.5
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    • pp.648-657
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    • 2002
  • This paper presents a numerical analysis on the solidification characteristics in twin-roll strip casting. Unstructured fixed-grid system was employed to deal with phase change. Melting of pure gallium was analyzed to confirm the validity of present program in both structured and unstructured grid systems. An algorithm for simultaneous calculation of the temperature in the roll and the molten metal pool was developed. The flow field in the pool and heat transfer features between pool and roll were shown. The effect of process parameters was also studied. Since the geometry of the molten metal Pool significantly deforms along the casting direction, unstructured grid system is more efficient. The unstructured grid system gives almost the same accuracy, even though the number of grids is only 60% of the structure done.

DEVELOPMENT OF CFD PROGRAM BASED ON A UNSTRUCTURED POLYHEDRAL GRID AND ITS APPLICATION TO FLOW AROUND A OSCILLATING CIRCULAR CYLINDER (비정렬 다면체 격자계 기반 유동 해석 프로그램의 개발 및 진동하는 실린더 주변 유동에의 적용)

  • Lee, Sang-Hyuk;Kang, Seong-Won;Hur, Nahm-Keon
    • 한국전산유체공학회:학술대회논문집
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    • 2011.05a
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    • pp.483-487
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    • 2011
  • In the present study, a CFD program based on a finite volume method was developed by using an unstructured polyhedral grid system for the accurate simulation with the complex geometry of computational domain. To simulate the transient flow induced by the moving solid object, the program used a fractional step method and a ALE (Algebric Lagrangian-Eulerian) method. The grid deformation for the moving of solid object were performed with a spring analogy based on the center coordinate of each computational grid. To verify the present program with these methodologies, the numerical results of the flow around the fixed and oscillating circular cylinder were compared with the previous numerical results.

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Viscous Flow Analysis around a Wind Turbine Blade with End Plate and Rake (풍력터빈 날개의 끝판과 레이크 효과에 대한 점성유동장 해석)

  • Kim, Ju-In;Kim, Wu-Joan
    • Journal of the Korean Society for Marine Environment & Energy
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    • v.14 no.4
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    • pp.273-279
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    • 2011
  • Turbulent flow analysis around a wind turbine blade was performed to evaluate the power performance of offshore wind turbine. Fluent package was utilized to solve the Reynolds-averaged Navier-Stokes equations in non-inertial rotating coordinates. The realizable k-$\varepsilon$ model was used for turbulence closure and the grid system combining structured and unstructured grids was generated. In the first, lift and drag forces of 2-D foil section were calculated and compared with existing experimental data for the validation. Then torque and thrust of the wind turbine blade having NACA 4-series sections were calculated with fixed pitch angle and rpm. Tip speed ratio was varied by changing wind speed. In the next, three kinds of end plate were attached at the tip of blade in order to increase the power of the wind turbine. Among them the end plate attached at the suction side of the blade was found to be most effective. Furthermore, performance analysis with tilt angle and rake was also performed.

The Limit of the Continuum Assumption Based on Compressible Flow Structures in an Axisymmetric Micro-Thruster Used for a Satellite (인공위성용 축대칭 소형 추력기의 압축성 유동 구조 계산에 의한 연속체 가정의 적용 한계)

  • Kwon, Soon-Duk;Kim, Sung-Cho;Kim, Jeong-Soo;Choi, Jong-Wook;Lee, Kee-Man
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.04a
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    • pp.281-285
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    • 2007
  • The flow characteristics in the thruster should be analyzed considering its geometry and the pressure ratio to estimate its performance and etc. This paper suggests the computational result of an axisymmetric real nozzle for the altitude control of a satellite to find out the application limit that the assumption of continuum mechanics holds. The steady non-reacted compressible flow field in the unstructured grid system is computed and analyzed with varying the environmental pressure (or the degree of vacuum) under the fixed pressure ratio in a real thruster of which the area ratio of exit to throat is 56. The assumption of the continuum mechanics is not approved when the environmental pressure is reduced less than $10^{-3}$ atm.

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