• 대한기계학회논문집B
• /
• 제33권6호
• /
• pp.435-442
• /
• 2009

Three-dimensional heat transfer characteristics for natural convection flows are numerically investigated in the doubly-inclined cubical-cavity according to the variation of a newly defined orientation angle �� of the hot wall surface from horizontal plane at moderate Rayleigh numbers. Numerical simulations of laminar flows are conducted in the range of Rayleigh numbers($10^4{\leq}Ra{\leq}10^5$) and $0^{\circ}{\leq}{\alpha}90^{circ}$ with a solution code(PowerCFD) employing unstructured cell-centered method. Comparisons of the average Nusselt number at the cold face are made with benchmark solutions and experimental results found in the literature. It is found that the average Nusselt number at the cold wall has a maximum value around the specified orientation ${\alpha}$ at each Rayleigh number. Special attention is also paid to three-dimensional thermal characteristics in natural convection according to new orientation angles at Ra��= $1{\times}10^5$, in order to investigate a new additional heat transfer characteristic found in the range of above Ra = $6{\times}10^4$.

• 대한기계학회논문집
• /
• 제5권4호
• /
• pp.329-337
• /
• 1981

Natural convection within inclined high aspect-ratio rectangular cavity was analysed by using finite element method. For a cavity of sapect-ratio 20, the flow patterns of secondary vortices and the heat transfer characteristics on the wall were obtained with the variation of tilt angle as well as Ra and Pr. The observation on the governing equations shows that the increase of Ra/Pr and the existence of nonzero tilt angle make the flow pattern more complicated and so it becomes difficult to obtain converging solution. The max. value of Ra/Pr attained in this study was 3x10$\^$4/at 0$\^$0/ tilt angle and 1.1x10$\^$4/ at 45.deg. tilt angle for aspect ratio 20and Pr=0.7. Finally an empirical formula for Nusselt number which can accout for the effect of tilt angle is obtained for laminar flow regime.

• Journal of applied mathematics & informatics
• /
• 제12권1_2호
• /
• pp.281-289
• /
• 2003

The convection of water is investigated in the vicinity of its density maximum temperature (277 K) in an inclined square cavity in the presence of heat sources. Numerical investigations are carried out by maintaining one of the vertical walls uniformly at 273 K and varying the other wall between temperatures 275 K and 285 K at different inclinations angles. The isotherms, streamlines and velocity profiles reveal the possible existence of multicellular fluid motions, and bidirectional velocity distributions. These fluid flow and heat transfer characteristics are significantly modified by the cavity inclination in the presence of heat sources.

• 한국연소학회지
• /
• 제12권2호
• /
• pp.20-25
• /
• 2007

The supersonic combustion experiments are carried out using T3 free-piston shock tunnel. Hydrogen Fuel is injected in the cavity parallel with air(or nitrogen) flow. The equivalence ratios in this study are 0.132 and 0.447. Experimental measurements use OH-PLIF near the cavity and pressures in the combustor. For parallel fuel injection case, direct fuel add into cavity leads to increase of cavity pressure. And Flame exists just near the bottom wall for low equivalent ratio. There is no flame in the cavity because of no mixing in it. Compared to the inclined fuel injection, ignition delay length is longer for low equivalence ratio in both case. OH distribution is not a single line but a repeatable fluctuation flame structure by turbulence. Pressure distributions have nothing to do with the fuel injection position.

• 한국연소학회:학술대회논문집
• /
• 한국연소학회 2007년도 제34회 KOSCO SYMPOSIUM 논문집
• /
• pp.31-36
• /
• 2007

The supersonic combustion experiments are carried out using T3 free-piston shock tunnel. Hydrogen Fuel is injected in the cavity parallel with air(or nitrogen fuel) flow. The equivalence ratios in this study are 0.132 and 0.447. Experimental measurements use OH-PLIF near the cavity and pressures in the combustor. For parallel fuel injection case, direct fuel add into cavity leads to increase of cavity pressure. And Flame exists just near the bottom wall for low equivalent ratio. There is no flame in the cavity because of no mixing in it. Compared to the inclined fuel injection, ignition delay length is longer for low equivalence ratio in both case. OH distribution is not a single line but a repeatable fluctuation flame structure by turbulence. Pressure distributions have nothing to do with the fuel injection position.

• Journal of Advanced Marine Engineering and Technology
• /
• 제33권8호
• /
• pp.1180-1186
• /
• 2009

이 실험적인 연구는 오픈 캐비티에서 경사후방벽면을 가지고 있는 유동장안의 제어봉이 있고 없음과 제어봉의 위치에 따른 유동 내부특성을 알고자 하였다. 속도 측정법으로는 흐름과 입자 영상의 가시화가 가능한 PIV기법을 이용하여 레이놀즈수의 변화와 속도에 대하여 고찰하였다. 제어봉의 어느 위치가 캐비티 내부유동 특성에 영향을 적게 주며, 전단 혼합 층이 유동장 상부와 하류 쪽으로 이동하는지에 대한 레이놀즈수의 임계점을 알고자 하였다.그 결과, 제어봉의 위치 L/H=0.2에서, 제어봉의 위치를 각각 상이하게 정하여 보았으나, L/H=0.2의 경우가 가장 캐비티에 영향을 적게 주는 것으로 판단된다. 주와류 후방의 흐름이 상부로 서서히 치우쳐 있으며 레이놀즈수가 증가할수록 이러한 현상은 뚜렷해지고, 이것은 y/H=1.0 전후의 주 흐름은 제어봉의 효과로 캐비티 상부에 발생한 주 와류의 위쪽으로 치우쳐 하류로 진행하기 때문으로 판단된다. 이러한 현상은 레이놀즈수가 증가하면서 더욱 뚜렷해지며 그 임계점은 $Re=1.0{\times}10^4$전후임을 알 수 있었다. 제어봉의 위치가 L/H=0.1의 경우 레이놀즈수의 증가 ($Re=6.0{\times}10^3$, $Re=8.0{\times}10^3$, $Re=1.0{\times}10^4$, $Re=1.2{\times}10^4$)에 따라 상부에 이중와류 구조가 발생하고, 캐비티 상부의 전단 혼합 층이 증가함에 따라 하단부의 속도분포가 더 안정적인 모습도 알 수 있었다.

• 한국추진공학회지
• /
• 제23권3호
• /
• pp.76-87
• /
• 2019

공동형 화염 안정화 장치를 갖는 초음속 연소기를 직접 연결 방식으로 시험을 수행하였다. 고도 20 km, 비행 마하수 4에 해당하는 전온도, 전압력 유동 조건에 대해 액체 탄화 수소 연료를 경사 분사와 공력 램프 분사의 2가지 방법으로 분사하였다. 축방향 벽면 압력과 연소기 출구의 전압력을 계측하여 연료량에 따른 연소 특성을 파악하였다.

• 대한기계학회논문집
• /
• 제17권2호
• /
• pp.458-466
• /
• 1993

Natural convection in trapezoidal sections of cavity was numerically investigated using a Finite Volume Method. Temperatures of the upper inclined and lower horizontal walls are constant, with vertical side walls being insulated. When the top wall is hotter than the bottom one, a single cell of stratified flow field is obtained and heat transfer occurs only by conduction. For the colder top wall, bifurcation solutions are obtained for the higher Rayleigh numbers, while unique solutions for lower values. Flow structure is strongly dependent on the configuration and the Rayleigh number.

• 한국추진공학회지
• /
• 제13권4호
• /
• pp.9-15
• /
• 2009

스크램제트 엔진의 연소기 내부 유동은 초음속이므로 유동의 잔류시간과 혼합율의 증대가 효과적인 연소를 가능하게 하는 주요 요인으로 작용한다. 본 연구에서는 연료-공기 혼합기로써 L/D=4.8인 개방형 공동 모델을 사용하였고, 공동 앞에서의 경사 연료 분사 시 분사구 주위와 공동 주위의 유동특성을 살펴보기 위하여 레이저 슐리렌 기법과 압력측정을 실시하였다. 측정에 사용된 레이저 슐리렌은 10 ns의 매우 짧은 광원 지속시간을 보유하여 공동부근의 비정상 유동 현상을 효과적으로 관찰할 수 있었다. 압력측정은 연료 분사비 J(운동량비)를 변화시켜 가며 측정하였으며, 운동량비에 따른 연소기 내부 주요 압력상승 지점의 변화를 살펴 볼 수 있었다.

• 설비공학논문집
• /
• 제9권4호
• /
• pp.435-445
• /
• 1997

It was studied the phenomena of transient freezing of an inclined water-saturated enclosure. One side of the test section was cooled and the other sides were insulated. The effects of the initial temperature, the inclination angle on the temperature field and the shape of the ice-water interface were observed. In the beginning of freezing, with increasing the inclination angle the freezing rate was increased and in the stable density layer centered $4^{\circ}C$, the freezing was fast as the convective fluid flow became small. When the initial temperature was above the $4^{\circ}C$, the frozen thickness in the upper part of inclined surface was thinner than that in the lower part, but with time the frozen thickness of upper part was thicker than that of lower part, below the $4^{\circ}C$, the frozen thickness in the upper part was thicker than that of lower part from the begining, and above the $8^{\circ}C$ in the beginning upper part was thinner with concave, but with time thicker the upper part, vanishing concave.