• Wind and Structures
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• 제18권5호
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• pp.511-528
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• 2014

The characteristics of wake galloping phenomenon for two parallel/unparallel circular cylinders were investigated via wind tunnel tests. The two cylinders were initially deployed in parallel and wake galloping phenomena were observed by varying the center-to-center distance. The effect of an unparallel arrangement of two cylinders was next investigated by fixing the spacing ratio of one side of the cylinders at 5.0D and the other side at 3.0D, in which D represents the diameter of the cylinder. For the unparallel disposition, the 5.0D side showed a small, limited vibration while the 3.0D side produced much larger amplitude of vibration, resulting in a rolling motion. However, the overall amplitude appeared to decrease in unparallel disposition when compared with the amplitude of the 3.0D - 3.0D parallel case. This represents the mitigation effect of wake galloping due to the unparallel disposition between two cylinders. Flow visualization tests with particle image velocimetry were conducted to identify flow fields between two cylinders. The test results demonstrate the existence of a complex interaction of the downstream cylinder with the shear layer generated by the upstream cylinder. When the spacing ratio was large enough, the shear layer was not observed and the downstream cylinder showed only limited random vibration.

• Structural Engineering and Mechanics
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• 제83권4호
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• pp.495-513
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• 2022

This paper aims to study the fracture mechanism of rocks under the 'u'shape cutters considering the effects of crack (pre-existing crack) distances, crack spacing and crack inclination angles. The effects of loading rates on the rock fragmentation underneath these cutters have been also studied. For this purpose, nine experimental samples with dimensions of 5 cm×10 cm×10 cm consisting of the non-persistent cracks were prepared. The first three specimens' sets had one non-persistent crack (pre-existing crack) with a length of 2 cm and angularity of 0°, 45°, and 90°. The spacing between the crack and the "u" shape cutter was 2 cm. The second three specimens" set had one non-persistent crack with a length of 2 cm and angularity of 0°, 45°, and 90° but the spacing between pre-existing crack and the "u" shape cutter was 4 cm. The third three specimens'set has two non-persistent cracks with lengths of 2 cm and angularity of 0°, 45° and 90°. The spacing between the upper crack and the "u" shape cutter was 2 cm and the spacing between the lower crack and the upper crack was 2 cm. The samples were tested under a loading rate of 0.005 mm/s. concurrent with the experimental investigation. The numerical simulations were performed on the modeled samples with non-persistent cracks using PFC2D. These models were tested under three different loading rates of 0.005 mm/s, 0.01 mm/sec and 0.02 mm/sec. These results show that the crack number, crack spacing, crack angularity, and loading rate has important effects on the crack growth mechanism in the rocks underneath the "u" shape cutters. In addition, the failure modes and the fracture patterns in the experimental tests and numerical simulations are similar to one another showing the validity and accuracy of the current study.

• 한국ITS학회 논문지
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• 제23권1호
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• pp.82-96
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• 2024

교통류에서는 거시적인 지표로 속도, 교통량, 밀도가 중요한 파라미터로 활용되고 있으며, 미시적인 지표로는 가속도와 차두거리가 중요한 파라미터로 활용되고 있다. 속도와 교통량은 현재 설치된 교통정보 수집장치로 수집이 가능하지만 가속도와 차두거리는 안전과 자율주행분야 등에 필요성이 있지만 현재 교통정보 수집장치로는 수집이 불가능한 실정이다. 객체인식 기법인 YOLO는 정확도와 실시간성이 우수하여 교통분야를 포함하여 다양한 분야에서 활용되고 있다. 본 연구에서는 YOLO를 활용하여 가속도와 차두거리를 측정하기 위해 측정 간격을 조밀하게 설정하여 간격별 차량의 속도 변화와 차량 간 통행시간 차이를 통해 가속도와 차두거리를 측정하는 모델을 개발하였다. 지점별 교통특성에 따라 가속도와 차두거리의 범위가 다름을 확인하였고, 측정률 확보를 위한 기준거리와 화면각도에 따른 비교분석을 수행하다. 측정간격은 20m, 각도는 직각에 가까울수록 측정률이 높아짐을 분석하였다. 이를 통해 교차로별 안전도 분석과 국내 차량행태모델 분석에 기여할 수 있을 것이다.

• 대한기계학회논문집B
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• 제26권8호
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• pp.1115-1122
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• 2002

The present experiment investigates the effects of pore density f of aluminum foam heat sinks, the jet-to-jet spacing X and the nozzle plate-to-target surface spacing H of 3$\times$3 square impinging arrays on the averaged Nusselt number. The performance of the aluminum foam heat sinks and the rectangular plate heat sink is evaluated in terms of the enhancement factor. /equation omitted/. The multiple impinging jet with X/d=4.0 displays higher Nusselt numbers than single impinging jet for 12.0$\leq$H/d$\leq$20.0. With the variation of the jet-to-jet spacing, the aluminum foam heat sink of 10 PPI show higher Nusselt numbers than the 20 and 40 PPI aluminum foam heat sinks. Further, the 10 PPI aluminum foam heat sink demonstrates 26% higher enhancement factor than the rectangular plate heat sink in the range of 7000$\leq$Re$\leq$11000.

• Advances in aircraft and spacecraft science
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• 제10권3호
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• pp.203-222
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• 2023

The detonation combustion is a supersonic combustion process follows on shock wave oscillations in detonation tube. In this paper numerical studies are carried out combined effect of blockage ratio and spacing of obstacle on detonation wave propagation of hydrogen-air mixture in pulse detonation combustor. The deflagration to detonation transition of stoichiometric (ϕ=1)fuel-air mixture in channel has been analyzed for effect of blockage ratio (BR)=0.39, 0.51, 0.59, 0.71 with spacing of 2D and 3D. The reactive Navier-Stokes equation is used to solve the detonation wave propagation mechanism in Ansys Fluent platform. The result shows that fully developed detonation wave initiation regime is observed near smaller vortex generator ratio of BR=0.39 inside the combustor. The turbulent rate of reaction has also a great significance role for shock wave structure. However, vortices of rapid detonation wave are appears near thin boundary layer of each obstacle. Finally, detonation combustor demonstrates the superiority of pressure gain combustor with turbulent rate of reaction of 0.6 kg mol/m3 -s inside the detonation tube with obstacle spacing of 12 cm, this blockage enhanced the turbulence intensity and propulsive thrust. The successful detonation wave propagation speed is achieved in shortest possible time of 0.031s with a significance magnitude of 2349 m/s, which is higher than Chapman-Jouguet (C-J) velocity of 1848 m/s. Furthermore, stronger propulsive thrust force of 36.82 N is generated in pulse time of 0.031s.

• 대한기계학회논문집
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• 제12권3호
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• pp.561-565
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• 1988

본 연구에서는 제어함수를 수식으로부터 유도하여 자동적인 격자간격제어가 가능한 "근사직교 경계고정곡선좌표계"를 생성하는 새로운 방법을 제시하여 2차원영역 에 대한 그 적용을 논의하고자 한다. 논의하고자 한다.

• 대한기계학회논문집B
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• 제31권1호
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• pp.8-15
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• 2007

The jet impingement cooling characteristics are investigated experimentally. The study is motivated by the potential application of local hot spot cooling by means of the vortex tube. The purposes of this research are to examine the effect of the nozzle-block spacing and flow rate. The results of jet through vortex tube is compared with ones of circular Jet. Flow visualization by the smoke-wire technique is also performed to investigate the flow structure. As the nozzle-block spacing is increased and flow rate decreased, the cooling effect of the Jet through the vortex tube decreases mere remarkably than that of the circular jet. So the cooling effect for the jet through the vortex tube is higher than that for the circular jet at $H/D{\leq}3$, $Q{\geq}10m^3/h$.

• Journal of electromagnetic engineering and science
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• 제13권4호
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• pp.240-244
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• 2013

In this paper, we present an improvement of a closed-form formula for mutual impedance computation. Depending on the center-to-center spacing between two rectangular microstrip patch antennas, the mutual impedance formula is separated into two parts. The formula based on synthetic asymptote and variable separation is utilized for spacings of more than 0.5 ${\lambda}_0$. When the spacing is less than 0.5 ${\lambda}_0$, an approximate formula is proposed to improve the computation for closely spaced elements. Simulation results are compared to computational results of mutual impedances and mutual coupling coefficients as functions of normalized center-to-center spacing in both E- and H-plane coupling configurations. A good agreement between simulation and computation is achieved.

• 터널과지하공간
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• 제23권1호
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• pp.42-53
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• 2013

천공 작업 시 드릴비트 버튼의 타격 속도와 타격 간격은 천공효율을 높이는데 있어 매우 중요한 요소이다. 따라서 본 연구에서는 버튼의 타격 속도 및 간격에 따른 암반 파쇄성능을 분석하기 위하여 홉킨스바 시험기를 이용한 타격시험을 수행하였다. 먼저, 버튼의 타격속도에 따른 암석파쇄 현상을 분석하기 위하여 단일타격 시험을 수행하였고, 수치해석을 통해 단일 타격 시험에 대한 암석의 파쇄과정을 모사하였다. 다음으로 버튼의 타격 간격에 따른 천공효율을 예측하기 위하여 타격 후 설정된 거리만큼 암석 시료를 이동시키고 재차 타격하는 방식으로 다중타격 시험을 수행하였다. 타격시험 후 암석의 천공부피는 레이저 스캐너를 이용하여 측정하였으며, 타격에너지와 천공부피를 통해 천공성능을 계산하였다. 이러한 시험 결과를 바탕으로 직경 102 mm 드릴비트의 1회 타격 시 천공성능을 예측하였다.

• 대한기계학회논문집
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• 제16권8호
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• pp.1566-1574
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• 1992

본 연구에서는 원형수직 충돌분류에 의한 가열평판의 전열특성을 해석하기 위 하여 최근 표면온도 측정에 많이 사용되고 있는 liquid crystal을 이용하였다. 즉 liquid crystal의 감온특성과 영상처리 기법을 이용하여 레이놀즈수 및 노즐과 충돌판 사이의 거리(L/D) 변화에 따른 전열면의 온도장 변화를 측정하였다.