• 제목/요약/키워드: 아격자스케일 모델

검색결과 5건 처리시간 0.016초

난류유동의 Large-Eddy Simulation 기법의 알고리즘 향상에 관한 연구 (Improvement on Large-Eddy Simulation Technique of Turbulent Flow)

  • 앙경수
    • 대한기계학회논문집
    • /
    • 제19권7호
    • /
    • pp.1691-1701
    • /
    • 1995
  • Two aspects of Large-Eddy Simulation(LES) are investigated in order to improve its performance. The first one is on how to determine the model coefficient in conjunction with a dynamic subgrid-scale model, and the second one is on a wall-layer model(WLM) which allows one to skip near-wall regions to save a large number of grid points otherwise required. Especially, a WLM suitable for a separated flow is considered. Firstly, an averaging technique to calculate the model coefficient of dynamic subgrid-scale modeling(DSGSM) is introduced. The technique is based on the concept of local averaging, and useful to stabilize numerical solution in conjunction with LES of complex turbulent flows using DSGSM. It is relatively simple to implement, and takes very low overhead in CPU time. It is also able to detect the region of negative model coefficient where the "backscattering" of turbulence energy occurs. Secondly, a wall-layer model based on a local turbulence intensity is considered. It locally determines wall-shear stresses depending on the local flow situations including separation, and yields better predictions in separated regions than the conventional WLM. The two techniques are tested for a turbulent obstacle flow, and show the direction of further improvements.rovements.

높은 레이놀즈수에서의 난류 장애물유동의 Large-Eddy-Simulation (Large-Eddy Simulation of a Turbulent Obstacle Flow at a High Reynolds Number)

  • 양경수
    • 대한기계학회논문집
    • /
    • 제18권7호
    • /
    • pp.1866-1872
    • /
    • 1994
  • Turbulent flow in a channel with a square rib periodically mounted on one wall is studied by large-eddy simulation(LES). An efficient 3D Navier-Stokes solver has been written for this geometry using a fractional step method and a multi-grid technique. The Reynolds number considered is 82, 000 based on the mean velocity above the obstacle height. Near-wall turbulence is approximated by a wall-layer model based on the turbulence intensity at the grid point nearest a solid wall. The results show a good qualitative agreement with experiments currently available for a single rib, indicating that LES can be a useful tool in simulating complex turbulent flows.

홈이 파진 평판 사이 난류유동의 대와동모사 (LES) (Large eddy simulation of turbulent flows in a grooved channel)

  • 양경수;김도형
    • 대한기계학회논문집B
    • /
    • 제22권1호
    • /
    • pp.34-49
    • /
    • 1998
  • In this study, turbulent flows in a grooved channel are numerically investigated by Large Eddy Simulation (LES). Especially, a parametric study is carried out to study effects of length and depth of a groove on large-scale flow structures. For one test case, comparison of LES results with those of DNS reveals a good agreement even though the number of grid points of LES is only 6.5% of that of DNS. This confirms that LES is a suitable tool for a parametric study of turbulent flows. The subsequent parametric study using LES shows that the large-scale turbulent structures are significantly affected by the geometry of the groove. Especially, when the length of the groove is short such that the recirculation region occupies the entire groove, the turbulent flow in the groove becomes very weak in both mean and fluctuation quantities.

Planar-Jet형 연소기 내 난류유동의 LES (Large-Eddy Simulation of Turbulent Flows in a Planar Combustor)

  • 김도형;양경수;신동신
    • 대한기계학회논문집B
    • /
    • 제24권10호
    • /
    • pp.1409-1416
    • /
    • 2000
  • In this study, turbulent flows in a planar combustor which has a square rib-type flame holder are numerically investigated by Large Eddy Simulation(LES). Firstly, the flow fields with or without jet injection downstream of the flame-holder are examined using uniform inlet velocity. Comparison of the present LES results with experimental one shows a good agreement. Secondly, to investigate mixing of oxidizer(air) and fuel injected behind the flame holder, the scalar-transport equation is introduced and solved. From the instantaneous flow and scalar fields, complex and intense mixing phenomena between fuel and jet are observed. It is shown that the ratio of jet to blocked air velocity is an important factor to determine the flow structure. Especially, when the ratio is large enough, the fuel jet penetrates the main vortices shed from the flame holder, resulting in significant changes in the flow and scalar fields.

사각 덕트내 난류 횡단류 유동장에 분사되는 액체 제트의 분열과 미립화에 관한 LES 해석 (LES on breakup and atomization of a liquid jet into cross turbulent flow in a rectangular duct)

  • 유영린;한두희;성홍계;전혁수;박철현
    • 한국항공우주학회지
    • /
    • 제44권4호
    • /
    • pp.290-297
    • /
    • 2016
  • 사각덕트에서 난류 유동장으로 분사되는 액체 제트의 액주 분열과 미립화 현상에 관한 LES를 수행하였다. 기체상태의 공기 유동 해석에 오일러리안 해법을 사용하고, 액적 추적을 위하여 라그랑지안 해법을 사용하여 기체-액체간 이상유동(two phase flow) 해석을 수행하였다. 액적 분열 모델, 아격자 스케일 모델 및 공간 차분법에 따른 액적 분열을 조사하였다. 액체 제트의 침투깊이를 경험식과 비교하였으며 경험식보다 약간 높음을 알 수 있었다. 제트 후류에서 사우터 평균직경에 대한 분석을 수행하였다.