• Structural Engineering and Mechanics
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• 제71권6호
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• pp.713-738
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• 2019

In the paper the dynamics of the oscillating moving load acting in the interior of the hollow cylinder surrounded with elastic medium is studied within the scope of the exact field equations of 3D elastodynamics. It is assumed that the oscillating load act on the certain arc of the internal circle of the cylinder's cross section and this load moves with constant velocity along the cylinder's axis. The corresponding 3D dynamic problem is solved by employing moving coordinate system, the exponential Fourier transform and the presentation these transforms with the Fourier series. The expressions of the transforms are determined analytically, however their originals are found numerically. Under the investigations carried out in the paper the main attention is focused on the so-called "gyroscopic effect", according to which, the influence of the vibration frequency on the values of the critical velocity and interface stresses are determined. Numerical results illustrated this effect are presented and discussed. In particular, it is established how the non-axisymmetricity of the problem acts on the influence of the load oscillation on its critical velocity and on the interface stresses.

• 한국기후변화학회지
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• 제8권1호
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• pp.11-19
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• 2017

This study examined the relationship between the initiation timing typhoon season in the Northwestern Pacific and the tropical sea surface temperature (SST) using a numerical simulation. The initiation timing of the typhoon season is closely associated with SSTs over the Indian Ocean (IO) and the eastern Pacific (EP) in the preceding winter and early-spring. The experiment based on the Weather and Research Forecast (WRF) model showed that the start date of the typhoon season is delayed for about one month when the SSTs over the IO and the EP increase in the preceding winter. The forced tropical SST pattern induces anticyclonic anomalies in the Northwestern Pacific, which is an unfavorable condition for typhoon development, and hence it could delay the initiation of the typhoon season.

• 한국가시화정보학회지
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• 제22권1호
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• pp.6-17
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• 2024

This study examined the natural convection heat flow characteristics of the melting process of PCM (palm oil) inside a liquid flexitank(bag) for a cargo container. A film heating element was installed on the bottom of the container, and numerical analysis was performed under heat flux conditions of 1,000 to 4,000 W/m². As a result, the melt interface of the PCM rises to a nearly horizontal state over time. In the initial stage, conduction heat transfer dominates, but gradually waves at the cell flow and melt interfaces are formed due to natural convection heat transfer. As melting progresses, the Ra number increases parabolically, and the Nu number increases linearly and has a constant value. The Nu number rises slowly under low heat flux conditions, whereas under high heat flux conditions, the Nu number rises rapidly. As the heat flux increases, the internal temperature oscillation of the liquid phase after melting increases. However, under high heat flux conditions, excess heat exceeding the latent heat is generated, and the temperature of the molten liquid is raised, so the increase in melting rate decreases. Therefore, the appropriate heating element specification applied to a 20-ton palm oil container is 2,000 W/m².

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2003년도 제20회 춘계학술대회 논문집
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• pp.91-93
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• 2003

A comprehensive numerical study is carried out to investigate for the understanding of the flow evolution and flame development in a supersonic combustor with normal injection of ncumally injecting hydrogen in airsupersonic flows. The formulation treats the complete conservation equations of mass, momentum, energy, and species concentration for a multi-component chemically reacting system. For the numerical simulation of supersonic combustion, multi-species Navier-Stokes equations and detailed chemistry of H2-Air is considered. It also accommodates a finite-rate chemical kinetics mechanism of hydrogen-air combustion GRI-Mech. 2.11[1], which consists of nine species and twenty-five reaction steps. Turbulence closure is achieved by means of a k-two-equation model (2). The governing equations are spatially discretized using a finite-volume approach, and temporally integrated by means of a second-order accurate implicit scheme (3-5).The supersonic combustor consists of a flat channel of 10 cm height and a fuel-injection slit of 0.1 cm width located at 10 cm downstream of the inlet. A cavity of 5 cm height and 20 cm width is installed at 15 cm downstream of the injection slit. A total of 936160 grids are used for the main-combustor flow passage, and 159161 grids for the cavity. The grids are clustered in the flow direction near the fuel injector and cavity, as well as in the vertical direction near the bottom wall. The no-slip and adiabatic conditions are assumed throughout the entire wall boundary. As a specific example, the inflow Mach number is assumed to be 3, and the temperature and pressure are 600 K and 0.1 MPa, respectively. Gaseous hydrogen at a temperature of 151.5 K is injected normal to the wall from a choked injector.A series of calculations were carried out by varying the fuel injection pressure from 0.5 to 1.5MPa. This amounts to changing the fuel mass flow rate or the overall equivalence ratio for different operating regimes. Figure 1 shows the instantaneous temperature fields in the supersonic combustor at four different conditions. The dark blue region represents the hot burned gases. At the fuel injection pressure of 0.5 MPa, the flame is stably anchored, but the flow field exhibits a high-amplitude oscillation. At the fuel injection pressure of 1.0 MPa, the Mach reflection occurs ahead of the injector. The interaction between the incoming air and the injection flow becomes much more complex, and the fuel/air mixing is strongly enhanced. The Mach reflection oscillates and results in a strong fluctuation in the combustor wall pressure. At the fuel injection pressure of 1.5MPa, the flow inside the combustor becomes nearly choked and the Mach reflection is displaced forward. The leading shock wave moves slowly toward the inlet, and eventually causes the combustor-upstart due to the thermal choking. The cavity appears to play a secondary role in driving the flow unsteadiness, in spite of its influence on the fuel/air mixing and flame evolution. Further investigation is necessary on this issue. The present study features detailed resolution of the flow and flame dynamics in the combustor, which was not typically available in most of the previous works. In particular, the oscillatory flow characteristics are captured at a scale sufficient to identify the underlying physical mechanisms. Much of the flow unsteadiness is not related to the cavity, but rather to the intrinsic unsteadiness in the flowfield, as also shown experimentally by Ben-Yakar et al. [6], The interactions between the unsteady flow and flame evolution may cause a large excursion of flow oscillation. The work appears to be the first of its kind in the numerical study of combustion oscillations in a supersonic combustor, although a similar phenomenon was previously reported experimentally. A more comprehensive discussion will be given in the final paper presented at the colloquium.

• 대한토목학회논문집
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• 제32권3B호
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• pp.175-183
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• 2012

본 연구에서는 천수방정식에 Galerkin법과 Petrov-Galerkin 기법의 일종인 SU/PG 기법을 적용하여 유한요소 천수흐름 해석 모형을 개발하고, 다양한 실험수로에서 이송이 지배적인 흐름을 수치 모의하였다. 수로 내부에 얇은 판 형태의 구조물이 존재하는 경우 Fr 수와 Re 수가 매우 낮은 흐름에서는 Galerkin 기법과 SU/PG 기법이 동일한 결과를 나타냈으나, Fr=1.58인 경우 Galerkin법은 발산하여 해를 얻을 수 없었다. 이 경우 SU/PG법은 Newton-Raphson법에 의한 5회의 반복에 의해 수렴된 유속결과를 구할 수 있었다. 사류와 상류가 혼재하여 천이류가 나타나는 단면확대 수로 모의에서 SU/PG 기법을 이용한 본 연구의 경우 상류단 수심조건이 잘 유지되며, 도수가 발생하는 지점 및 도수에 의한 수심 경사, 도수 후의 수심이 모두 Khalifa(1980)의 실험결과와 매우 근사하였다. 이송이 지배적인 사류(Fr=2.74)에 의한 사각도수 모의의 경우에도 Galerkin 기법은 최초 모의시간의 첫 번째 반복 이후 발산하였으나, SU/PG 기법은 도수 경계면을 수치진동 없이 잘 포착하였으며, 해석해와 비교한 수심 및 유속의 최대 오차는 0.2% 이내로 나타나 기존 연구(Levin 등, 2006; Ricchiuto 등, 2007)에 비해 더욱 정확한 결과를 도출하였다.

• 한국안광학회지
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• 제13권1호
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• pp.5-13
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• 2008

목적: 각막 부착 콘택트렌즈에는 어떠한 힘이 작용하며 또한 이 힘에 따른 렌즈의 운동을 알아보고자 본 해설을 작성하였다. 방법: 렌즈 아래 눈물층에는 모세관작용에 따른 힘이 발생하고 렌즈 회전에 따른 눈물층 간격변화에 기인하는 복원력이 발생한다. 눈깜빡임에 따라 콘택트렌즈는 눈꺼풀-렌즈 사이 마찰력과 눈꺼풀의 가속도에 의한 힘, 눈물층의 복원력 및 점성저항력에 의해 운동(움직임)이 결정된다. 눈깜빡임 도중/후 매순간 렌즈의 위치를 예측할 수 있는 미분방정식과 그 수치계산 프로그램 모델을 수립하였다. 이 컴퓨터 모델을 사용하여 눈깜빡임 주기, 렌즈의 BC, 눈꺼풀 압력 변화에 따른 매 순간 렌즈 위치를 예측할 수 있었다. 결과: 눈깜빡임 주기가 길수록, 눈꺼풀 압력이 클수록 눈꺼풀에 의한 마찰력 영향이 커져 렌즈 움직임이 커지며 BC가 증가할수록 눈물층 간격이 증가하여 점성저항력이 감소하며 따라서 렌즈 움직임이 커지는 것을 알 수 있었다. 눈깜빡임 후 렌즈는 눈물층 간격 변화에 따른 복원력과 눈물층의 점성저항력에 의해 진폭이 감소하는 진동을 하면서 평형위치로 복귀하게 된다. 이 경우 BC가 증가할수록 저항력이 감소하여 평형 위치로의 접근이 빨라진다. 결론: 콘택트렌즈의 움직임은 렌즈-각막 사이 눈물층의 물성 및 형상과 아울러 눈깜빡임에 의해 지배된다.

• 대한기계학회논문집B
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• 제36권2호
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• pp.181-188
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• 2012

대향류확산화염의 화염소화에 있어서 에지화염 역할에 관한 실험적 연구가 진행되었다. 속도비, 버너직경, 그리고 버너간격을 변화시키며 수행된 실험에서 전체신장률에 따른 화염소화 임계질소몰분율의 그래프는 c-커브 형태로 나타났다. 고신장률화염에서는 화염소화 임계질소몰분율의 그래프가 하나의 곡선으로 일치하였으며, 화염이 일차원의 응답특성을 갖는 것을 확인하였다. 화염 소화는 바깥 에지화염이 반경방향으로의 진동 후에 화염 중심으로 수축하며 소화하는 영역, 진동 없이 화염중심으로 수축하며 소화하는 영역, 그리고 바깥 에지부분의 수축과 진동 없이 화염중심에 화염 구멍이 생기며 소화하는 영역으로 세 가지 모드로 나타났다. 화염 표면온도 측정과 에너지 방정식의 각항을 수치해석 한 결과를 토대로 에지화염부분에서의 반경방향 전도 열손실이 에지화염의 불안정을 야기한다는 것과 전도를 통한 열 공급뿐만 아니라 대류를 통한 열 공급도 바깥 에지화염의 안정화에 기여한다는 것을 보였다. 그리고 반경방향의 전도열손실이 수축하며 소화하는 메커니즘의 지배적인 역할을 함을 보였다.

• 한국해양학회지:바다
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• 제27권2호
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• pp.49-70
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• 2022

해수면 온도는 기후와 바다의 생태계 그리고 인간의 활동에까지 중요한 영향을 미치는 해수의 특성 중 하나로 이를 예측하는 것은 항상 중요하게 다뤄지는 문제다. 최근 들어 과거의 패턴을 학습하여 예측값을 생성할 수 있는 딥러닝을 활용한 해수면 온도 예측이 복잡한 수치모델을 이용한 예측의 대안으로 주목받고 있다. 딥러닝은 입력 자료 간의 비선형적인 관계를 추정할 수 있는 것이 큰 장점이며, 최근 컴퓨터 그래픽카드의 발달로 많은 양의 데이터를 반복적이고 빠르게 계산할 수 있게 되었다. 본 연구에서는 기존의 딥러닝 모델의 단점들을 보완하면서 시공간 자료를 다룰 수 있는 합성곱 신경망(Convolutional Neural Network) 기반의 U-Net을 통해 단기 해수면 온도 예측을 수행하였다. 개발한 딥러닝 모델을 이용한 한국 남부 근해 해수면 온도의 단기 예측은 예측일의 해수면 온도의 중장기 변동성에 따라 달라지는 성능을 보였다. 해수면 온도 변동성의 증감은 계절적 변동 뿐 아니라 Pacific Decadal Oscillation (PDO) 지수의 변동과도 유의미한 상관관계를 보였는데, 이는 계절 변동 및 PDO에 따른 기후 변화에 기인한 수온 전선의 강도 변화가 해수면 온도의 시공간적 변동성에 영향을 줌으로써 발생했음을 확인하였다. 본 연구는 해수면 수온 자료가 가지고 있는 계절적 변동성과 경년 변동성이 딥러닝 모델의 해수면 단기 수온 예측 성능에 기여함을 밝힌 것에 그 의의가 있다.

• 수산해양기술연구
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• 제43권1호
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• pp.49-61
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• 2007

Otter boards in the trawl are the one of essential equipments for the net mouth to be spread to the horizontal direction. Its performance should be considered in the light of the spreading force to the drag and the stability of towing in the water. Up to the present, studies of the otter boards have focused mainly on the drag and lift force, but not on the stability of otter boards movement in 3 dimensional space. In this study, the otter board is regarded as a rigid body, which has six degrees of freedom motion in three dimensional coordinate system. The forces acting on the otter boards are the underwater weight, the resistance of drag and spread forces and the tension on the warps and otter pendants. The equations of forces were derived and substituted into the governing equations of 6 degrees of freedom motion, then the second order of differential equations to the otter boards were established. For the stable numerical integration of this system, Backward Euler one of implicit methods was used. From the results of the numerical calculation, graphic simulation was carried out. The simulations were conducted for 3 types of otter boards having same area with different aspect ratio(${\lambda}=0.5,\;1.0,\;1.5$). The tested gear was mid-water trawl and the towing speed was 4k't. The length of warp was 350m and all conditions were same to each otter board. The results of this study are like this; First, the otter boards of ${\lambda}=1.0$ showed the longest spread distance, and the ${\lambda}=0.5$ showed the shorted spread distance. Second, the otter boards of ${\lambda}=1.0$ and 1.5 showed the upright at the towing speed of 4k't, but the one of ${\lambda}=0.5$ heeled outside. Third, the yawing angles of three otter boards were similar after 100 seconds with the small oscillation. Fourth, it was revealed that the net height and width are affected by the characteristics of otter boards such as the lift coefficient.

• Smart Structures and Systems
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• 제22권5호
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• pp.495-508
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• 2018

Shape memory alloys (SMAs) exhibit superelasticity given the ambient temperature is above the austenite finish temperature threshold, the magnitude of which significantly depends on the metal ingredients though. For the monocrystalline CuAlBe SMAs, their superelasticity was found being maintained even when the ambient temperature is down to $-40^{\circ}C$. Thus this makes such SMAs particularly favorable for outdoor seismic applications, such as the framed structures located in cold regions with substantial temperature oscillation. Due to the thermo-mechanical coupling mechanism, the hysteretic properties of SMAs vary with temperature change, primarily including altered material strength and different damping. Thus, this study adopted the monocrystalline CuAlBe SMAs as the kernel component of the SMA braces. To quantify the seismic response characteristics at various temperatures, a wide temperature range from -40 to $40^{\circ}C$ are considered. The middle temperature, $0^{\circ}C$, is artificially selected to be the reference temperature in the performance comparisons, as well the corresponding material properties are used in the seismic design procedure. Both single-degree-of-freedom systems and a six-story braced frame were numerically analyzed by subjecting them to a suite of earthquake ground motions corresponding to the design basis hazard level. To the frame structures, the analytical results show that temperature variation generates minor influence on deformation and energy demands, whereas low temperatures help to reduce acceleration demands. Further, attributed to the excellent superelasticity of the monocrystalline CuAlBe SMAs, the frames successfully maintain recentering capability without leaving residual deformation upon considered earthquakes, even when the temperature is down to $-40^{\circ}C$.