• 대한기계학회논문집
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• 제12권4호
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• pp.847-864
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• 1988

본 연구에서는 연료분출에 박리가 있는 경우와 없는 경우 각각에 대하여 화염 대 근처의 국부가속 현상이 박리에 의하여 어떻게 영향을 받는가를 실험적으로 규명하 고, 나아가서 종래에 행해져 왔던 관련 연구 결과를 재검토할려고 한다.

• 대한기계학회논문집B
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• 제25권5호
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• pp.722-730
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• 2001

The local heat transfer of an axisymmetric submerged air jet impinging on a heated flat plate is investigated experimentally with the variation of mesh-screen solidity. The screen installed in front of the nozzle exit modifies the flow structure and local heat transfer characteristics. The mean velocity and turbulence intensity profiles of streamwise velocity component are measured using a hot-wire anemometry. The temperature distribution on the heated flat surface is measured with thermocouples. The smoke-wire flow visualization technique was employed to understand the near-field flow structure qualitatively for different mesh screens. Large-scale toroidal vortices and high turbulence intensity enhance the heat transfer rate in the stagnation region. For a higher solidity, turbulence intensity become higher which increases the local heat transfer at small nozzle-to-plate spacings such as L/D<6. The local and average Nusselt numbers of impinging jet from the $\sigma$(sub)s=0.83 screen at L/D=2 are about 5.6∼7.5% and 7.1% larger than those for the case of no screen, respectively. For the nozzle-to-plate spacings larger than 6, however, the turbulence intensities for all tested screens approach to an asymptotic curve and the mean velocity along the jet centerline decreases monotonically. As the nozzle-to-plat spacing increases for high solidity screens, the heat transfer rate decreases due to the reduction in turbulence intensity and jet momentum.

• 한국항공우주학회지
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• 제47권2호
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• pp.81-89
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• 2019

본 연구는 쿼드 틸트 프로펠러(Quad Tilt Propeller)형상의 탠덤날개 항공기의 전진비행 조건을 풍동실험하여 전방 날개 및 프로펠러가 후방날개에 작용하는 공력 간섭효과를 분석하였다. 6축 밸런스시스템을 이용해 전기체의 힘을 측정하였고 날개뿌리에 부착된 스트레인게이지를 이용하여 각 날개의 굽힘모멘트를 측정하였다. 12홀 프로브를 이용해 날개 및 프로펠러 후류의 유동장을 측정하였으며, 털실과 스모크를 이용한 유동가시화 실험을 통해 유동 특징을 정성적으로 확인하였다. 요소별 공력간섭 현상을 측정하기 위해 프로펠러 부착 조합을 바꿔가며 전방날개와 프로펠러가 후방날개에 작용하는 영향을 분석하였다.

• 한국컴퓨터그래픽스학회논문지
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• 제14권4호
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• pp.27-33
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• 2008

물리기반 레픽스 기술은 연기 물, 화염과 같은 자연현상을 계산 물리학으로 시뮬레이션하고 이를 가시화하는 기술이다. 본 논문에서는 시뮬레이션 된 다수의 파티클 유체데이터를 사각 스플렛을 이용하여 3차원으로 빠르게 가시화 하는 기법을 제안한다. SPH(Smoothed Paticle hydrodynamic) 기법을 사용하여 스플렛의 위치와 법선 벡터를 계산하고, 단적 현상을 줄이 기 위해 사각뿔 형상으로 스플렛을 재구성하고 가시화 한다. SPH 기법을 사용하는 유체 시뮬레이션 엔진에 적용하여 자연스러운 물의 유동 현상을 성공적으로 가시화 하였다.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2004년도 제29회 KOSCI SYMPOSIUM 논문집
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• pp.85-90
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• 2004

We have presented characteristics of a transitional behavior from a premixed flame to a triple flame in a lifted flame according to the change of equivalence ratio. The experimental apparatus consisted of a slot burner and a contraction nozzle for a lifted flame. As concentration difference of the both side of slot burner increases, the shape of flame changed from a premixed flame to a triple flame, and the liftoff height is decreased to the minimum value and then increase again. Around this minimum point, it is confirmed a transition regime from premixed flame to triple flame. Consequently, the experimental results of the liftoff height, flame curvature and luminescence intensity showed that the stabilized laminar lifted flame regime is categorized by regimes of premixed flame, triple flame and critical flame. In the visualization experiment of smoke wire, the flow divergence and redirection reappeared in premixed flame as well as triple flame. Thus we cannot express the flame front of lifted flame has a behavior of triple flame with only flow divergence and redirection. To differentiate triple flame and premixed flame, ${\Phi}$ value of partially premixed fraction is employed. The partially premixed fraction ${\Phi}$ was constant in premixed flame. In critical flame small gradient appears over the whole regime. In triple flame, typical diffusion flame shape is obtained as parabolic distribution type due to diffusion flame trailing.

• International Journal of Internet, Broadcasting and Communication
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• 제16권2호
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• pp.237-246
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• 2024

In recent years, the frequent occurrence of fire accidents in university libraries has posed significant threats to the safety of students' lives and property, alongside negative social impacts. Accurately analyzing the factors affecting evacuation during library fires and proposing optimized measures for safe evacuation is thus crucial. This paper utilizes a specific university library as a case study, simulating fire evacuation scenarios using the Pathfinder software, to assess and validate evacuation strategies and propose relevant optimizations. Pathfinder, developed by Thunderhead Engineering in the United States, is an intuitive and straightforward personnel emergency evacuation assessment system, offering advanced visualization interfaces and 3D animation effects. This study aims to construct evacuation models and perform simulation analysis for the selected university library using Pathfinder. The library's structural layout, people flow characteristics, and the nature of fire and smoke spread are considered in the analysis. Additionally, evacuation scenarios involving different fire outbreak locations and the status of emergency exits are examined. The findings underscore the importance of effective evacuation in fire situations, highlighting how environmental conditions, individual characteristics, and behavioral patterns significantly influence evacuation efficiency. Through these investigations, the study enhances understanding and optimization of evacuation strategies in fire scenarios, thereby improving safety and efficiency. The research not only provides concrete and practical guidelines for building design, management, and emergency response planning in libraries but also offers valuable insights for the design and management of effective evacuation systems in buildings, crucial for ensuring occupant safety and minimizing loss of life in potential hazard situations

• 대한기계학회논문집B
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• 제27권8호
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• pp.1023-1032
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• 2003

The effect of local forcing on the separated flow over a backward-facing step is investigated through hot-wire measurements and flow visualization with multi-smoke wires. The boundary layer upstream of the separation point is laminar and the Reynolds number based on the free stream velocity and the step height is 13800. The local forcing is given from a slit located at the step edge and the forcing signal is always defined when the wind tunnel is in operation. In case of single frequency forcing, the streamwise velocity and the reattachment length are measured under forcing with various forcing frequencies. For the range of 0.010〈S $t_{\theta}$〈0.013, the forcing frequency component of the streamwise velocity fluctuation grows exponentially and is saturated at x/h = 0.75 , while its subharmonic component grows following the fundamental and is saturated at x/h = 2.0. However, the saturated value of the subharmonic is much lower than that of the fundamental. It is observed that the vortex formation is inhibited by the forcing at S $t_{\theta}$ = 0.019 . For double frequency forcing, natural instability frequency is adopted as a fundamental frequency and its subharmonic is superposed on it. The fundamental frequency component of the streamwise velocity grows exponentially and is saturated at 0.5 < x/ｈ < 0.75, while its subharmonic component grows following the fundamental and is saturated at x/ｈ= 1.5 . Furthermore, the saturated value of the subharmonic component is much higher than that for the single frequency forcing and is nearly the same or higher than that of the fundamental. It is observed that the subharmonic component does not grow for the narrow range of the initial phase difference. This means that there is a range of the initial phase difference where the vortex parring cannot be enhanced or amplified by double frequency forcing. In addition, this effect of the initial phase difference on the development of the shear layer and the distribution of the reattachment length shows a similar trend. From these observations, it can be inferred that the development of the shear layer and the reattachment length are closely related to the vortex paring.

• 한국항공우주학회지
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• 제34권12호
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• pp.1-8
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• 2006

진동하는 에어포일의 후류에 미치는 레이놀즈수의 영향을 조사하기 위한 실험적 연구를 수행하였다. NACA 0012 에어포일은 1/4 시위를 기준으로 피칭운동을 하고, $\pm$6$^{\circ}$ 내에서 진동하도록 설정하였다. 진동하는 에어포일에서 후류를 측정하기 위하여 2축 열선풍속계가 사용되었고 연선 가시화 기법이 경계층을 관찰하기 위하여 사용되었다. 실험조건에서 자유흐름속도는 1.98, 2.83 그리고 4.03 m/s이며, 이를 근거로 한 레이놀즈수는 각각 $2.3{\times}10^4$, 3.3${\times}10^4$, 4.8${\times}10^4$이다. 모든 경우에 에어포일 진동수는 무차원 진동수 K=0.1에 맞게 조절되었다. 실험 결과, 피칭하는 에어포일의 경계층 및 후류 유동 특성은 레이놀즈수 2.3$\times$104, 3.3$\times$104 사이에서 크게 다르게 나타나며, 레이놀즈수 3.3${\times}10^4$와 4.8${\times}10^4$에서 유사하게 나타난다. 이것은 레이놀즈수 2.3$\times$104에서 비정상 분리가 크게 지연되기 때문이다.

• 한국가스학회지
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• 제2권1호
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• pp.28-39
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• 1998

본 연구에서는 $20\%$ 천장개구부가 있는 정사각형 밀폐공간내의 순수자연대류와 자연대류 -복사가 고려된 복합열전달을 순차해석과 실험을 통하여 비교 분석하였다. 수치해석은 순수자연대류에 대하여 SIMPLE 알고리즘을 사용하였고, 복사열전달에 대해서는 S-N 구분 종좌표법을 이용하였으며 난류유동의 경계조건은 벽함수를 적용하였다. 실험은 수치해석의 결과와 비교하기 위하여 동일한 조건에 대하여 수행되었다. 그 결과 순수자연대류와 복합열전달의 유동장, 온도장의 형상은 유사한 유선함수를 보이고 있으며, 유동가시화를 통한 실험결과와 잘 일치하고 있음을 보여준다. 수치해석과 실험의 온도분포를 비교한 결과 평균 $8.5\%$의 오차를 보였다.