• Title/Summary/Keyword: snappyHexMesh

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NUMERICAL INVESTIGATION OF SHOCK-BUFFET ON TRANSPORT AIRCRAFT WITH CHANGING THE POSITION OF NACELLE/PYLON (항공기 Nacelle/pylon 위치에 따른 Shock-Buffet 현상의 수치적 연구)

  • Kim, S.H.;Yee, K.J.;Oh, S.J.
    • Journal of computational fluids engineering
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    • v.19 no.3
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    • pp.69-76
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    • 2014
  • The shock buffet on a transonic transport aircraft are negative factors that reduce the aerodynamic performance of aircraft. The parametric studies were performed for position of nacelle/pylon to estimate the trend of flow mechanism under the wing that affects shock buffet. To generate external mesh of aircraft configuration that change the position of nacelle, snappyHexMesh provided in OpenFOAM was applied. Implicit density-based solver(ISAAC) was used for flow analysis. The change of nacelle position along horizontal direction dynamically affected the aerodynamic performance of transonic transport aircraft as comparing that of vertical direction. As a result of the parametric study of nacelle/pylon position, it was confirmed that the optimal position of nacelle can be obtained by aerodynamic design.

COMPUTATION OF FLOW AROUND A SHIP USING A SURFACE INTERPOLATED FROM STATION LINES (선체 횡단면 곡선 보간에 의한 표면 생성 및 유동 계산)

  • Kim, Hyun-Sik;Shin, Sangmook
    • Journal of computational fluids engineering
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    • v.20 no.4
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    • pp.21-27
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    • 2015
  • Flow field around the KRISO 3600TEU container ship is computed using a surface generated based on interpolations of station lines, which are given in a body plan of the ship, without using any CAD program. An interpolation method is suggested based on inscribed circles to generate curves between two neighboring station lines. The interpolated surface is saved in a STL format to use the snappyHexMesh utility of the openfoam. Computed resistance of the ship is compared with experimental and other computational results and the effects of the interpolation of neighboring station lines on the computed resistance are investigated. The suggested method is applied to calculate the flow field around a submarine with appendages. The surface triangulations for the hull and the appendages are generated without consideration of each other, then those surface triangulations are simply combined to provide a grid generator with the body boundary. The junctures of the hull and the appendages are identified automatically during the grid generation procedure. Tip vortex is captured, which travels downstream from the tip of the appendages.