• 제목/요약/키워드: turbulent energy

검색결과 770건 처리시간 0.028초

2차원 분류특성에 관한 연구 (A Study on The Characteristics of the 2-Dimensional Jet)

  • 김경훈;박상규
    • 한국정밀공학회지
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    • 제6권4호
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    • pp.43-51
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    • 1989
  • Free jet was investigated experimentally and numerically in range of Reynolds number from 9900 to 21000. The working fluid was air; the mean velocity components and turbulent quantities were measured by a hot-wire anemometer. In numerical computations, the governing partial differential equations of elliptic type were solved with conventional k- ${\epsilon}$ turbulence model. The measurements show that the jet increased linearly in flow direction, and that similarity for each turbulent quantity such as Reynolds shear stress, or turbulent kinetic energy was revealed in the fully developed region. The computational results show good agreements with experiments.

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Escape of LyC and Lyα Photons from Simulated Turbulent Clouds

  • 김태선
    • 천문학회보
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    • 제44권1호
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    • pp.73.2-73.2
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    • 2019
  • Understanding how ionizing radiation propagates from molecular clouds to the intergalactic space is the key to the study of reionization and the emergence of $Ly{\alpha}$ emission from galaxies. In this contribution, I will present our new efforts to better understand the escape of UV photons from turbulent clouds with different masses, star formation efficiencies, and spectral energy distributions using radiation-hydrodynamic simulations. I will also show predicted Lya profiles from turbulent clouds and discuss a few interesting differences identified when compared with the properties of the local green pea galaxies.

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전부하 운전조건에서 메탄올 개질연료를 사용한 가솔린 엔진의 연소특성에 대한 수치해석 (A Numerical Analysis on Combustion Characteristics of the Gasoline Engine using Methanol Reformulated Fuels under WOT Condition)

  • 이석영;전충환
    • 에너지공학
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    • 제20권2호
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    • pp.163-169
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    • 2011
  • 기관의 구조를 변경하지 않는 상태에서 RM50의 사용 가능성에 대한 결정을 하기 위해 수치해석을 수행하였다. 열발생률을 비교한 결과 기관회전수가 증가할수록 각 연료간의 차이가 감소하였으며, RM50, 가솔린의 순서로 열발생률의 최대치가 높음을 알 수 있었다. 이는 연료의 연소속도의 순서와 동일하였다. 난류연소속도는 RM50이 가장 높으며 난류강도의 곡선은 난류 연소속도 곡선과 비슷한 경향을 보이고 있으며 RM50이 다른 연료에 비해 연소속도가 빠르고 소염거리가 짧으므로 연소실의 온도가 높아 NO 배출물을 증가시키는 요인이 되지만 NO의 화학적 반응 동력학의 영향에 의해 결과적으로 NO 배출물을 감소시킨다. 따라서 RM50 연료의 사용 가능성을 예측할 때는 연료의 저위발열량에 의한 실린더내 온도뿐 만 아니라 연소속도를 포함한 연소특성까지 고려할 필요가 있다.

높은 레이놀즈수를 가진 난류 진동 경계층에서의 k-ε과 k-ω 난류모형의 비교 (Comparative Study on k-ε and k-ω Closures under the Condition of Turbulent Oscillatory Boundary Layer Flow at High Reynolds Number)

  • 손민우;이관홍;이길성;이두한
    • 한국수자원학회논문집
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    • 제44권3호
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    • pp.189-198
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    • 2011
  • 본 연구는 난류현상의 모형화를 위해 널리 이용되는 k-$\varepsilon$과 k-$\omega$ 난류모형을 비교하는 것이 목적으로, 횡방향 흐름이 무시될 수 있는 U-튜브 모양의 터널형 수로 내 높은 레이놀즈수를 가진 진동 경계층 흐름에 두 난류해석방법을 적용하였다. 난류모형의 적용은 1차원 연직 모형을 통해 이루어지며, 수치 모의 결과, 유속의 분포와 난류운동에너지 (turbulent kinetic energy) 모두에서 두 모형이 매우 유사한 결과를 나타낸다. 이를 통하여, 횡방향 압력경사가 무시될 수 있는 조건에서는 k-$\varepsilon$과 k-$\omega$ 난류모형이 큰 차이를 보이지 않고, 우수한 결과를 나타냄을 알 수 있다. 따라서 직선형 하천 및 하구부, 해안에서의 파랑 흐름 등과 같이 횡방향의 압력경사가 미미한 지역에서의 난류를 수치적으로 해석할 경우, 기존의 풍부한 연구를 통해 매개변수의 검보증이 장기간 이루어진 k-$\varepsilon$ 모형을 이용하는 것이 추천된다.

수평 과냉 . 난류액막류의 막비등 열전달에 관한 연구 (Study on Film-Boiling Heat Transfer of Subcooled Turbulent Liquid Film Flow on Horizontal Plate)

  • 김영찬;서태원
    • 설비공학논문집
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    • 제12권9호
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    • pp.835-842
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    • 2000
  • Film boiling heat transfer of the subcooled turbulent liquid film flow on a horizontal plate was investigated by theoretical and experimental studies. In the theoretical analysis, by solving the integral energy and momentum equations analytically, some generalized expressions for Nusselt number was deduced. Next, by comparing the deduced equations with the experimental data on the turbulent film boiling heat transfer of the subcooled thin liquid film flow, the semi-empirical relation between the Nusselt number based on the modified heat transfer coefficient and the Reynolds number was obtained. The correlating equation was very similar to that of the turbulent heat transfer in a single phase flow, and it was found that the heat transfer was dissipated to increase the liquid temperature.

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전자기력을 이용한 난류경계층 제어 (Turbulent boundary layer control via electro-magnetic forces)

  • 이중호;성형진
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2004년도 춘계 학술대회논문집
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    • pp.166-171
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    • 2004
  • Direct numerical simulations are peformed to investigate the physics of a spatially developing turbulent boundary layer flow suddenly subjected to spanwise oscillating electro-magnetic forces in the near-wall region. The Reynolds number based on the inlet momentum thickness and free-stream velocity is $Re_\theta=300$. A fully-implicit fractional step method is employed to simulate the flow. The mean flow properties and the Reynolds stresses are obtained to analyze the near-wall turbulent structure. It is found that skin-friction and turbulent kinetic energy can be reduced by the electro-magnetic forces. Instantaneous flow visualization techniques are used to observe the response of streamwise vortices to spanwise oscillating forces. The near-wall vortical structures are clearly affected by spanwise oscillating electro-magnetic forces.

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DOHC 가솔린기관의 연소실 난류특성이 기관성능에 미치는 영향에 관한 연구 (A Study on the Influence of Turbulent Intensity on DOHC Engine Performance)

  • 김철수;최영돈
    • 한국자동차공학회논문집
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    • 제2권2호
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    • pp.12-23
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    • 1994
  • In order to investigate the effect of turbulent intensity on combustion characteristics, new flame factor model was developed. The principal study is the evaluation of interaction of swirl, tumble and unstrutural component of flow characteristics and correlation between turbulent intensity and flame factor. Computational and experimental study has been, performed such as quasi-dimensional cycle simulation, three dimensional flow analysis, engine performance test and diagnostic simulation. From these studies, it was found that flame factor was a function of engine speed and turbulent intensity.

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벽근방의 3각주에 의하여 교란받는 난류경계층에 관한 연구 (Study on the Turbulent Boundary Layer Disturbed by a Triangular Prism near the Wall)

  • 심우건;이강주;조용철
    • 설비공학논문집
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    • 제3권3호
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    • pp.161-167
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    • 1991
  • This paper presents the results of some measurement of the fluctuating velocity field in the turbulent boundary layer disturbed by a triangular prism and discusses the discovery of the disturbed boundary layer. A prism of height 8mm was used for experiments. The streamwise location of the prism was fixed at 1200mm downstream from the leading edge and the space between the prism center and the wall was set at three different values, 6, 15 and 33.5mm. The results show that the near-wall region of the disturbed boundary layer recovers original state much more quickly than the outer region. In the case h=6mm the recovery is faster than the other cases. Moreover, it was found that peak of fluctuating velocities moves outwards somewhat rapidly with increasing ${\times}$ mainly due to the turbulent diffusion of the fluctuating velocity.

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회전하는 원형단면 실린더 주위의 저 레이놀즈수 난류유동에 대한 직접수치모사 (Direct Numerical Simulation of Turbulent new Around a Rotating Circular Cylinder at Low Reynolds Number)

  • 황종연;양경수
    • 대한기계학회논문집B
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    • 제29권10호
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    • pp.1083-1091
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    • 2005
  • Turbulent flow around a rotating circular cylinder is investigated by Direct Numerical Simulation. The calculation is performed at three cases of low Reynolds number, Re=161, 348 and 623, based on the cylinder radius and friction velocity. Statistically strong similarities with fully developed channel flow are observed. Instantaneous flow visualization reveals that the turbulence length scale typically decreases as Reynolds number increases. Some insight into the spacial characteristics in conjunction with wave number is provided by wavelet analysis. The budget of dissipation rate as well as turbulent kinetic energy is computed and particular attention is given to the comparison with plane channel flow.

선회류 유입에 대한 원추디퓨저의 정압회복 특성 (The characteristics of static pressure recovery in a conical diffuser with a swirling flow)

  • 정효민;정한식
    • 대한기계학회논문집B
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    • 제22권7호
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    • pp.937-945
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    • 1998
  • The purpose of this paper is to investigate the relationship between pressure recovery and turbulent characteristic value of velocity and pressure, in the case where a swirling flow streams into a conical diffuser. The results of both measurements of the wall pressure fluctuation and velocity fluctuation revealed them to role the large part of the total pressure loss of the flow. The cause of the fluctuation of flow was showed to be the flow separation at the inlet of diffuser at low intensity of swirl, but the flow of diffuser center was instable at high intensity of swirl. The static pressure recovery depends strongly on the magnitude of the turbulent energy in the diffuser, and that this magnitude of the turbulent energy varies as the intensity of swirl at the diffuser inlet.