• 한국전산유체공학회지
• /
• 제9권3호
• /
• pp.26-38
• /
• 2004

A study has been made for the investigation of the robustness and convergence of various implicit operators of the LU-SGS scheme using linear stability analysis. It is shown that the behavior of the implicit operator is not determined by its own characteristics, but is determined relatively depending on the dissipative property of the explicit operator. It is also shown that, as the dissipation level of the implicit operator increases, the robustness of the scheme increases, but the convergence rate can be deteriorated due to the excessive dissipation. The numerical results demonstrate that the dissipation level of the impliict operator needs to be higher than that of the explicit operator for computing stiff problems.

• Wind and Structures
• /
• 제5권2_3_4호
• /
• pp.369-378
• /
• 2002

The application of Large Eddy Simulation (LES) in a curvilinear coordinate system to the flow around a square cylinder is presented. In order to obtain sufficient resolution near the side of the cylinder, we use an O-type grid. Even with a curvilinear coordinate system, it is difficult to avoid the numerical oscillation arising in high-Reynolds-number flows past a bluff body, without using an extremely fine grid used. An upwind scheme has the effect of removing the numerical oscillations, but, it is accompanied by numerical dissipation that is a kind of an additional sub-grid scale effect. Firstly, we investigate the effect of numerical dissipation on the computational results in a case where turbulent dissipation is removed in order to clarify the differences between the effect of numerical dissipation. Next, the applicability and the limitations of the present method, which combine the dynamic SGS model with acceptable numerical dissipation, are discussed.

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2004년도 추계 학술대회논문집
• /
• pp.73-77
• /
• 2004

In the present study, an efficient and robust implicit operator for the LU-SGS method is proposed. Numerical experiments for supersonic flow are performed to demonstrate the performance of the proposed method.

• Journal of Mechanical Science and Technology
• /
• 제18권1호
• /
• pp.173-182
• /
• 2004

The present study has focused on numerical investigation on the flame structure, flame lift-off and stabilization in the partially premixed turbulent lifted jet flames. Since the lifted jet flames have the partially premixed nature in the flow region between nozzle exit and flame base, level set approach is applied to simulate the partially premixed turbulent lifted jet flames for various fuel jet velocities and co-flow velocities. The flame stabilization mechanism and the flame structure near flame base are presented in detail. The predicted lift-off heights are compared with the measured ones.

• Journal of Mechanical Science and Technology
• /
• 제19권3호
• /
• pp.913-923
• /
• 2005

The dynamic mixed model (DMM) combined with a box filter of Zang et. al. (1993) has been generalized for passive scalar transport and applied to large eddy simulation of turbulent channel flows with Prandtl number up to 10. Results from a priori test showed that DMM is capable of predicting both subgrid-scale (SGS) scalar flux and dissipation rather accurately for the Prandtl numbers considered. This would suggest that the favorable feature of DMM, originally developed for the velocity field, works equally well for scalar transport problem. The validity of the DMM has also been tested a posteriori. The results of the large eddy simulation showed that DMM is superior to the dynamic Smagorinsky model in the prediction of scalar field and the model performance of DMM depends to a lesser degree on the ratio of test to grid filter widths, unlike in the a priori test.

• 한국추진공학회지
• /
• 제3권3호
• /
• pp.31-39
• /
• 1999

OFO, FOF 삼중 충돌형 및 FOOF 이중 분리 충돌형 분무연소장의 3차원 수치해석을 통한 연소성능 예측 및 성능설계 방법에 대하여 고찰하였다. 예조건화 압축성 유동 지배방정식과 저 레이놀즈수 $\kappa$-$\varepsilon$ 2 방정식 난류모델을 바탕으로 LU-SGS 기법을 사용하여 시간적분 하였으며 분무과정은 DSF 방법을 사용하여 모사하였다. n-heptane 액적과 공기를 연료와 산화제로 하는 액체 추진기관 내에서의 분무 연소장을 계산하였으며 연소에서의 난류의 영향은 eddy 소산모델을 사용하여 모사하였다. 분무연소장의 특성과 연소성능이 비교되었으며, 계산 결과 FOF 삼중 충돌형 분사기의 성능이 가장 우수한 반면, OFO 삼중 충돌형 분사기의 성능이 가장 저조한 것으로 나타났다. 연소효율에 중대한 영향을 미치는 파라미터로는 운동량비에 따른 초기 분무 액적의 평균직경과 혼합효율임을 확인하였다. 연소효율은 초기 분무 액적의 평균직경과 반비례, 혼합효율에 비례하여 증가되며, 산화제/연료 혼합비도 비례하여 상승하나, 일정 운동량비 이상에서는 감소되는 것으로 나타났다. 각 분사기 형태에서 운동량비에 따른 연소효율의 변화는 혼합효율의 변화와 동일한 경향을 보이며 그 크기는 분무 액적의 평균직경에 밀접한 관계가 있음을 알 수 있었다.