• Journal of the Korea Convergence Society
• /
• v.11 no.8
• /
• pp.159-163
• /
• 2020

In this study, the flow analyses around according to the existence or non- existence of the trailer's deflector and the shapes were carried out. In the absence of a deflector, the kinetic energy of the turbulence behind the container also generates higher kinetic energy in a wider area than in the presence of a deflector, which adversely affects the vehicle's driving performance. As a trailer's wind deflector-free model has unstable flow rates around the trailer and high kinetic energy of turbulence than a model with a deflector, it can be thought that the increase of fuel economy can be expected by installing a deflector in the trailer. By applying the study result on flow analysis near trailer due to shape of wind deflector, this study is seen to be suitable for the aesthetic convergence.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.37 no.10
• /
• pp.955-966
• /
• 2009

DES method is applied to an axisymmetric base flow at supersonic mainstream. The model is based on the Spalart-Allmaras (S-A) turbulence model in the RANS mode, and is based on the subgrid scale model in the Large-eddy simulation (LES) mode. Accurate predictions of the base flowfield and base pressure are successfully achieved by using the DES methodology which is less expensive than LES. Flow properties at the edge of base, such as boundary layer thickness, momentum thickness and skin fraction are compared with Dutton et al [experimental data to proper prediction of base flowfiled. From the present results, The DES accurately resolves the physics of unsteady turbulent motions, such as shear layer rollup, large-eddy motions in the downstream region and small eddy motions inside the recirculating region. Moreover, The present results of using an empirical constant $C_{DES}$ of 1.2 shows good agreement with experimental data than conventional empirical constant $C_{DES}$ of 0.65.

• The Korean Journal of Rheology
• /
• v.2 no.1
• /
• pp.87-89
• /
• 1990

n차 유체모델을 사용하여 비뉴우톤성 난류계에서 Kolmogorov microscales를 연구하 였다. 뉴우톤성유체와 2차유체양 모델에 대해서는 같은 미세척도 운동(small scale motion) 의 dissipation energy 뿐만아니고 Kolmogorov microscales도 같은 값으로 유도되었으나 3 차 유체모델을 사용하는 경우에는 비뉴우톤성 유체의 특성이 얻어졌다.

• Journal of the KSME
• /
• v.27 no.5
• /
• pp.421-427
• /
• 1987

공력소음은 공기역학적 힘에 의해서나 또는 유동 내에서의 난류와 같은 유체운동에 의해서만 발 생되는 소리와 관계되며, 진동하는 바이올린 줄이나 확성기의 진동에 의해서 발생되는 즉, 고체 표면의 진동에 의해서 발생되는 고전적인 음향학과는 무관하다. 그리고 여기서는 주로 공력 소음문제를 다루되 자세하고 엄밀한 수학적 전개보다는, 간단한 실제적인 예를 들어서, 물리적 메카니즘을 가능한 한 자세히 기술하여 공력 소음의 이해를 돕고자 하였다. 또한 오래된 고전적 방법을 가능한 한 피하고 최근의 방법으로 설명하도록 하였다.

• Journal of the Korean earth science society
• /
• v.25 no.2
• /
• pp.87-93
• /
• 2004

To study the effect of cloud on the variabilities of turbulent fluxes over the flat terrain, we used the gradient method to analyze the dynamic and thermodynamic data from the meteorological 9-m mast (0.75, 3 and 9 m) in Villafria airport in Spain. The decrease of the surface wind speed is governed by cooling at the surface following the evening transition. The sensible heat flux and the momentum flux are increased with the dynamic factor rather than the thermodynamic factor, and the sensible heat flux was not affected by the thermal condition. The global radiation did not play an important role in the variation of the sensible heat flux in the cloudy day, but the atmospheric surface layer was characterized rather by the wind intensity.

• Proceedings of the Korea Water Resources Association Conference
• /
• 2020.06a
• /
• pp.89-89
• /
• 2020

본 연구에서는 GPU 가속화 기반의 Boussinesq 모형인 Celeris Advecnt에 수심 적분된 2차원 이송-확산방정식을 추가하여 인터렉티브 시스템 기반의 추적자 이동 모형을 개발하였다. Celeris Advent는 최초로 개발된 인터렉티브 시스템을 갖춘 Boussinesq 모형으로, 시뮬레이션 중에 사용자가 모형의 파라미터뿐 아니라 모델 도메인 내 수위 및 수심을 바꿀 수 있다. 이를 통해 사용자는 모의가 진행되는 도중에 모델의 안정성 및 효율성을 위해 시간 간격을 조정할 수 있을 뿐 아니라 방파제 설치 등과 같은 지형 변화를 고려하기 위해 도메인 내 격자별 수심을 조정할 수 있다. 본 연구에서는 연안에서의 추적자 이동 모의를 위해 Boussinesq 방정식과 더불어 이송-확산방정식을 풀이하는 추적자 이동 모형을 개발하였다. 추적자의 확산항의 경우 분자 자체의 확산과 더불어 쇄파에 따른 난류 확산을 고려하였다. 난류 확산계수는 슈미트 수를 1로 두어 와동점성계수와 동일하게 두었으며, 와동점성은 단순화된 형태의 쇄파모형을 고려하여 계산하였다. 쇄파모형의 고려로 인해 이송-확산방정식과 더불어 운동량 방정식에서도 쇄파에 따른 운동량 소산이 고려되었다. 마지막으로, 추적자 농도에 대한 인터렉티브 시스템을 추가하여, 모델 구동 중에도 사용자가 수심적분된 추적자 농도를 조정할 수 있도록 하였다. 기수행된 2개의 수리실험 조건과 관측값을 이용하여 벤치마크 테스트를 수행하였으며, 관측값과 대체로 일치하는 것을 확인하였다.

• Journal of the Korean earth science society
• /
• v.32 no.1
• /
• pp.46-56
• /
• 2011

The purpose of this paper is to evaluate the wind energy resources with high spatial resolution in Sunghak and Guduck mountains in Busan Metropolitan area under the various atmospheric stabilities. The numerical model used in this research is A2C (Atmosphere to CFD), mainly applied to assess the regional scale and microscale meteorological phenformin. Wind under the strong atmospheric stability moves around mountain side smoothly due to the strong potential energy. On the other hand, the cavity region on the lee side of mountain tends to be created and expanded as the atmospheric stability decrease. Annually the average distribution of wind power density, turbulence kinetic energy, and vertical wind shear help to explain quantitatively that wind resource near the northern side of Guduck mountain top is more suitable to establish wind energy complex than that in any other regions in the target area.

• Transactions of the Korean Society of Mechanical Engineers
• /
• v.8 no.5
• /
• pp.442-449
• /
• 1984

Turbulent jet flow has been studied in many ways; a plane jet, a rectangular jet, an annular jet, a round jet, a wall jet, a parallel jet, a valve jet, a cross jet, a slit jet and etc. In this report, a 45.deg. cross jet flow was tried by using two same dimensioned nozzels(dia..phi.20)which were set up at the exit of the subsonic wind tunnel. Each jet flows to the direction of 22.5.deg. to the axis of downstream of the mixed flow. The centerline of each jet meets at the distance of 217.3mm and their mixing flow could be imagined to develop beyond that distance, so the measurement was effectuated at X/X$_{0}$=1.2-1.5. The section of the mixed flow a elliptic circle which is formed by the 22.5.deg. inclined flows to the X direction. This experimental study aimed at the investigation of the turbulent mixing process of two jets; the mean velocities, the turbulent shear stresses, the correlation coefficients, and the momentum were respectively measured. The mean velocity distribution profiles of the down-stream component measured in the Y direction coincide well with the empirical equation of Gortler and those measured in the Z direction agree with the equation of H. Schlichting. Other mean velocities V over bar and W over bar components were randomly distributed. The higher values with same order of the intensity of turbulence were largely distributed at the central part of the flow. The momentum was decreased up to 70% by the shock losses and the development of intense turbulences, but it kept its value constantly beyond X/d=14. Two-channel hot-wire anemometer systems (model 1050 series), X-type hot-wire made of tungsten (dia. .phi.e.mu.m, long 3mm, model 0252 T5), a computer(model HP 9845B0, and a plotter (model HP 9872C) were used for the experiments and the analyses.s.

• 한국전산유체공학회:학술대회논문집
• /
• 2007.04a
• /
• pp.83-86
• /
• 2007

Turbulent flow analysis is conducted around the multi-stage launch vehicle including base region and detachment motion of strap-on boosters due to resultant aerodynamic forces and gravity is simulated. Aerodynamic solution procedure is coupled with rigid body dynamics for the prediction of separation behavior. An overset mesh technique is adopted to achieve maximum efficiency in simulating relative motion of bodies and various turbulence models are implemented on the flow solver to predict the aerodynamic forces accurately. At first, some preliminary studies are conducted to show the importance of base flow for the exact prediction of detachment motion and to find the most suitable turbulence model for the simulation of launch vehicle configurations. And then, developed solver is applied to the simulation of KSR-III, a three-stage sounding rocket researched in Korea. From the analyses, after-body flow field strongly affects the separation motions of strap-on boosters. Negative pitching moment at initial stage is gradually recovered and a strap-on finally results in a safe separation, while fore-body analysis shows collision phenomena between core rocket and booster. And a slight variation of motion is observed from the comparison between inviscid and turbulent analyses. Change of separation trajectory based on viscous effects is just a few percent and therefore, inviscid analysis is sufficient for the simulation of separation motion if the study is focused only on the movement of strap-ons.

• Journal of Energy Engineering
• /
• v.22 no.4
• /
• pp.399-405
• /
• 2013

The gas motion inside the engine cylinder plays a very important role in determining the thermal efficiency of an internal combustion engine. A precise information of in-cylinder three dimensional complex gas motion is crucial in optimizing engine design. Homogeneous charge compression ignition (HCCI) engine is a combustion concept, which is a hybrid between Otto and Diesel engine. The turbulent diffusion leads to increased rates of momentum, heat and mass transfer. The in-cylinder turbulence flow was found to affect the present HCCI combustion mainly through its influence on the wall heat transfer. This study investigates the effect of piston geometry shape on the turbulent flow characteristics of in-cylinder from the numerical analysis using the LES model and the results obtained can offer guidelines of the combustion geometries for better combustion process and engine performance.