• 대한기계학회논문집B
• /
• 제35권6호
• /
• pp.561-567
• /
• 2011

2 차원 비직교 형상에 대해 비정렬 삼각 격자를 이용하여 복사 열전달의 역해석을 수행하였다. 본 논문에서는 확산적으로 방사 및 반사를 하는 벽면으로 이루어진 형상 내부에 흡수 및 방사, 산란하는 매질이 채워져 있는 문제를 고려하였다. 유한체적법을 사용하여 복사전달 방정식을 계산하였고 이 때 얻은 입사복사량을 역해석의 측정 데이터로 사용하였다. 벽면의 방사율을 추정하기 위해 켤레구배법을 적용하였으며, 목적 함수를 최소화하는 과정을 통해 해를 구하였다. 측정값의 측정 오차가 추정 정확도에 미치는 영향을 살펴보았고, 비정렬 격자계의 성능을 확인하기 위해 정렬 격자계를 이용하여 얻은 결과와 비교해 보았다.

• 한국항공우주학회지
• /
• 제33권2호
• /
• pp.1-10
• /
• 2005

비정상 유동의 모사를 위한 병렬화된 비정렬 중첩격자기법을 개발하였다. 비정렬 격자계에서 효율적이고 강건하게 쓰일 수 있는 탐색방법과 병렬경계에서 유동적으로 변하는 데이터의 수를 처리할 수 있는 자료구조를 제안하였다. 격자계간의 정보전달을 위한 삽간경계면을 정의하였고, 공간상의 이차정확도를 유지하기 위한 삽간방법 및 물체내부에 위치하는 삽간점에 대한 처리방법을 제안하였다. 개발된 해석코드의 검증을 위해 Eglin/Pylon 형상에서 분리되는 스토어의 궤적을 해석하여 실험치와 비교하였고, 다 물체간의 상대운동이 있는 비정상유동의 적용을 위해 세 개의 스토어 분리에 대한 해석을 수행하였다.

• 한국전산유체공학회지
• /
• 제9권1호
• /
• pp.48-56
• /
• 2004

The numerical simulations with unstructured mesh by cell-centered and vertex-centered approaches were peformed for the quadrilateral and triangular meshes. For 2-D inviscid supersonic vortex flow, the simulation results and the analytic solution were compared and the accuracy was assessed. The calculation efficiency was measured by the parameter defined by the consumed CPU time multiplied by absolute error As a results, equilateral triangular mesh yielded the best accuracy and efficiency among the tested meshes. Cell-centered approach gives a little better efficiency than vertex - centered approach.

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2005년도 추계 학술대회논문집
• /
• pp.135-139
• /
• 2005

An unstructured overset mesh method has been developed for the simulation of unsteady viscous flow fields around multiple bodies in relative motion. For this purpose, a robust and fast search technique is proposed for both triangle and high-aspect quadrilateral cell elements. The interpolation boundary is defined for data communication between grid systems and an interpolation method is suggested for viscous and inviscid cell elements. This method has been applied to calculate the flow fields around 2-D airfoil including relative motion. Validation were made by comparing the predicted results with those of experiments or other researcher's numerical results. It was demonstrated that the present method is efficient and robust for the prediction of unsteady time-accurate flow fields involving multiple bodies in relative motion.

• 한국연소학회지
• /
• 제6권2호
• /
• pp.15-22
• /
• 2001

A pressure-based, unstructured finite volume method has been applied to couple the chemical kinetics and fluid dynamics and to capture effectively and accurately the steep gradient flame field. The pressure-velocity coupling is handled by two methodologies including the pressure-correction algorithm and the projection scheme. A stiff, operator-split projection scheme for the detailed nonequilibrium chemistry has been employed to treat the stiff reaction source terms. The conservative form of the governing equations are integrated over a cell-centered control volume with collocated storage for all transport variables. Computations using detailed chemistry and variable transport properties were performed for two laminar reacting flows: a counterflow hydrogen-air diffusion flame and a lifted methane-air triple flame. Numerical results favorably agree with measurements in terms of the detailed flame structure.

• 한국전산유체공학회지
• /
• 제11권2호
• /
• pp.1-7
• /
• 2006

An unstructured overset mesh method has been developed for the simulation of unsteady viscous flow fields around multiple bodies in relative motion. For this purpose, a robust and fast search technique is proposed for both triangle and high-aspect ratio quadrilateral cell elements. The interpolation boundary is defined for data communication between grid systems and an interpolation method is suggested for viscous and inviscid cell elements. This method has been applied to calculate the flow fields around 2-D airfoils involving relative motion. Validations were made by comparing the predicted results with those of experiments or other numerical results. It was demonstrated that the present method is efficient and robust for the prediction of unsteady time-accurate flow fields involving multiple bodies in relative motion.

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2006년도 추계 학술대회논문집
• /
• pp.51-56
• /
• 2006

Several high resolution schemes such as OSHER, MUSCL, SMART, GAMMA, WACEB and CUBISTA are applied to two typical test cases of a translation test and a collapsing water column problem for the accurate capturing of fluid interfaces. It is accomplished by implementing the high resolution schemes in the in-house CFD code(PowerCFD) for computing 3-D flow with an unstructured cell-centered method, which is based on the finite-volume technique and fully conservative. The calculated results are found to show that SMART scheme gives the best performance with respect to accuracy and robustness.

• 한국전산유체공학회지
• /
• 제18권2호
• /
• pp.41-48
• /
• 2013

Ice accretion on the solid surface is an importance factor in assessing the performance of aircraft and wind turbine blade. Changes in the external shape due to ice accretion can greatly deteriorate the aerodynamic performance. In this study, a three-dimensional upwind-type second-order positivity-preserving finite volume CFD scheme based on the unstructured mesh topology is developed to simulate two-phase flow in atmospheric icing condition. The code is then validated by comparing with NASA IRT experimental data on the sphere. The present results of the collection efficiency are found to be in close agreement with experimental data and show improvement near the stagnation region.

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2008년도 춘계학술대회논문집
• /
• pp.47-50
• /
• 2008

The unsteady vortical flow over ONERA 70-degree delta wing was simulated using RANS and DES flow solvers on hybrid unstructured meshes. A study of time accuracy is accomplished to determine the effects of time step and number of iteration in pseudo-time stepping on numerical solutions. The grid size test is also performed to demonstrate that DES can be used to capture more accurately the unsteady vortical flow features over RANS simulation.

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2007년도 춘계 학술대회논문집
• /
• pp.41-44
• /
• 2007

A large eddy simulation method with unstructured mesh is presented. Two explicit filtering procedures are adopted for reducing the aliasing error of the nonlinear convective term and measuring the level of subgrid scale velocity fluctuation, respectively. The developed subgrid scale model is basically an eddy viscosity model which depends on both local velocity fluctuation level and local grid scale. As a validation problem, the flows around a sphere of several Reynolds numbers are simulated and some characteristic quantities are compared to experimental data and numerical results in the literature.