• Wind and Structures
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• 제28권5호
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• pp.285-298
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• 2019

For super long-span bridges, the aerodynamic forces induced by the flow passing the box girder should be considered carefully. And the Reynolds number sensitively of aerodynamic characteristics is one of considerable issue. In the study, a numerical study on the Reynolds number sensitivity of aerodynamic characteristic (flow pattern, pressure distribution and aerodynamic forces) of a twin-box girder were carried out using large eddy simulation (LES) with the dynamic Smagorinsky-Lilly subgrid model. The results show that the aerodynamic characteristics have strong correlation with the Reynolds number. At the leading edge, the flow experiences attachment, departure, and reattachment stages accompanying by the laminar transition into turbulence, causing pressure plateaus to form on the surface, and the pressure plateaus gradually shrinks. Around the gap, attributing that the flow experiences stages of laminar cavity flow, the wake with alternate shedding vortices, and turbulent cavity flow in sequence with an increase in the Reynolds number, the pressures around the gap vary greatly with the Reynold number. At the trailing edge, the pressure gradually recovers as the flow transits to turbulence (the flow undergoes wake instability, shear layer transition-reattachment station), In addition, at relative high Reynolds numbers, the drag force almost does not change, however, the lift force coefficient gradually decreases with an increase in Reynolds number.

• 한국항공우주학회지
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• 제36권7호
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• pp.628-633
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• 2008

십자형 낙하산은 원형 낙하산에 비해 제작상의 이점과 비용상의 이점이 있지만, 비정상 상태의 조건에 대해 많은 제약을 가지고 있다. 본 연구는 십자형 낙하산의 단점을 개선하여 더 나은 형태의 낙하산을 개발하는데 목적을 두고 있으며, Reefing을 통해 이러한 단점들을 개선 할 수 있을 것이라 기대하고 있다. 공력 특성 중에 낙하산의 성능에 가장 크게 작용하는 항력, 안정성, 진동에 대해 풍동 시험을 진행 하였으며, Reefing 효과로 인해 변화되는 낙하산의 형태와 성능들에 대해 연구 할 수 있었다.공력 계수를 얻기 위한 풍동시험은 6분력 피라미달 밸런스와 전방 고정부에 설치된 로드셀에 의해 측정이 되었다. 4개의 십자형 낙하산을 제작하였고, 각각의 값들을 비교하였다. Reefing line ratio에 따라 공력계수들의 변화를 알 수 있었다. 또한 reefing 효과에 따라 separation edge가 발생되어 십자형 낙하산의 안전성 향상을 확인할 수 있었다. 본 연구를 통해 기존 십자형 낙하산의 단점인 안정성을 향상시켜 다양한 분야에서 새로운 십자형 낙하산이 사용될 것이라 기대된다.

• 한국전기전자재료학회논문지
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• 제21권7호
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• pp.669-673
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• 2008

ITO thin film was deposited on PC substrate in Facing Targets Sputtering (FTS) system with various sputtering conditions. After it is applied to external bending force, we investigated how change the surface and electrical property of as-deposited ITO thin film. As the L(face-plate distance) of substrate decreases, it found that the maximum crack density is increasing at the center position and decreasing crack density as goes to the edge. So to apply same curvature (r) and bending force to PC substrate with ITO thin film, we fixed the L that is equal to curvature radius (2r). Before bending test, ITO thin films that deposited in the input current of 0.4 A and thickness of 200 nm already had biaxial tensile failure because of each different CTE (Coefficient of Thermal Expansion) and Others had been shown no bending or crack. After bending test, all samples had been shown cracks at about 200 times and as increasing the crack density, resistivity increased.

• 한국정밀공학회지
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• 제9권4호
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• pp.147-153
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• 1992

This study was undertaken to investigate the cutting behaviour of super duralumin (A2024-T3) with sintered carbide tool(P20). The cutting test was carried out under different conditions such as cutting speed, cutting depth and rake angle, etc. The specific cutting force Kc and Kt of vertical and radial forces decreases as cutting speed increases, especially the decrease rate of Kt becomes larger than of Kc as cutting speed increases. Kc and Kt in small cutting depth are much affected by work-hardening of surface layer. The chip width and shear angle become layer as cutting depth increases, especially chip width at feed of 0.1mm almost approaches cutting width. Relation between the friction coefficient of chip side and tool rake angle side can make the modelization studying the built-up edge size. The shear angle model equation of super duralumin generally agree with theory of Ernst-Merchant.

• 한국항공우주학회지
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• 제40권12호
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• pp.1080-1085
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• 2012

본 논문에서는 작동유의 최대 동점성 계수가 400cSt까지 변하는 조건에서 항공기 도어 댐퍼용 칼날형 댐핑 오리피스를 설계하였다. 전산 유동 해석과 실험을 통하여 칼날 오리피스의 유량계수를 분석하였고, 오리피스의 크기와 칼날 각도, 유동방향, 레이놀즈수가 미치는 영향을 고려하였다. 이 결과를 바탕으로 오리피스의 크기에 따라 댐퍼의 성능 기준을 충족시키기 위해 제한해야 하는 댐퍼의 쿨롱 마찰력 범위를 유도하였다.

• Wind and Structures
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• 제34권1호
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• pp.81-90
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• 2022

To better understand the vortex-induced vibration (VIV) characteristics of a 5:1 rectangular cylinder, the distribution of aerodynamic force and the non-dimensional power spectral density (PSD) of fluctuating pressure on the side surface were studied in different VIV development stages, and their differences in the stationary state and vibration stages were analyzed. The spanwise and streamwise correlations of surface pressures were studied, and the flow field structure partitions on the side surface were defined based on the streamwise correlation analysis. The results show that the variation tendencies of mean and root mean square (RMS) pressure coefficients are similar in different VIV development stages. The RMS values during amplitude growth are larger than those at peak amplitude, and the smallest RMS values are observed in the stationary state. The spanwise correlation coefficients of aerodynamic lifts increase with increase of the peak amplitude. However, for the lock-in region, the maximum spanwise correlation coefficient for aerodynamic lifts occurs in the VIV rising stage rather than in the peak amplitude stage, probably due to the interaction of vortex shedding force (VSF) and self-excited force (SEF). The streamwise correlation results show that the demarcation point positions between the recirculation region and the main vortex region remain almost constant in different VIV development stages, and the reattachment points gradually move to the tailing edge with increasing amplitude. This study provides a reference to estimate the demarcation point and reattachment point positions through streamwise correlation and phase angle analysis from wind tunnel tests.

• 대한토목학회논문집
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• 제26권4B호
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• pp.413-420
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• 2006

연안역에 설치되는 구조물로서 경관이나 해수 교환면에서 높은 기능을 가지고 있는 수중방파제의 건설이 증가하고 있다. 수중방파제의 경우, 천단이 정수면 아래에 위치하기 때문에 소형선박의 항해에 대한 표식으로서 일반적으로 부이가 많이 이용되고 있으나, 경관면 뿐만 아니라 쇄파파력에 의한 계류시스템의 파단과 같은 문제점이 지적되고 있다. 이로 인해, 최근에는 계류부이방식 대신에 자연에 가까운 경관을 창조할 수 있는 표식암을 이용하는 경우가 늘고 있으며, 이러한 표식암에 작용하는 파력의 정확한 예측은 설계 시 매우 중요하다. 본 연구에서는 불규칙 파동장을 대상으로 표식암에 작용하는 파력특성을 수리모형실험에 근거하여 검토하였다. 무차원 파력은 수중방파제상의 표식암 설치위치가 연안측으로 이동함에 따라 감소하는 경향을 보였다. 또한, Morison식을 이용하여 얻어진 항력계수와 관성력계수의 변동특성이 K.C.수의 변화와 연관되어 논의되었다.

• 생물환경조절학회지
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• 제2권1호
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• pp.46-52
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• 1993

The wind pressure distributions were analyzed through the wind tunnel experiment to provide fundamental criteria for the structural design on the three-span arched house according to the wind directions. In order to investigate the wind force distribution, the variation of the wind force coefficients, the mean wind force coefficients, the drag force coefficients and the lift force coefficients were estimated from the experimental data. The results obtained are as follows : 1. The variation of the wind force with the wind directions on the side walls was the greatest at the upwind edge of the walls. The change of pressure from the positive to the negative on the side walls occurred at the wind direction of 30$^{\circ}$ in the first house and 60$^{\circ}$ in the third house. 2. The maximum negative wind force along the length of the roof appeared at the length ratio of 0-0.2, when the wind directions were 90$^{\circ}$ in the first house, 60$^{\circ}$ in the second house and 30$^{\circ}$ in the third house. 3. The maximum negative wind force along the width of the roof appeared at the width ratio and the wind direction of 0.4 and 0$^{\circ}$ in the first house, 0.4-0.6 and 30$^{\circ}$ in the second house and 0.6 and 30$^{\circ}$ in the third house, respectively. 4. The maximum mean positive and negative wind forces occurred at the wind direction of 60$^{\circ}$ and 30$^{\circ}$, respectively, on the side walls of the first house, and the maximum mean negative wind force on the roof occurred at the wind direction of 30$^{\circ}$ in third house. 5. The maximum drag and lift forces occurred at the wind direction of 30$^{\circ}$, and the maximum lift force appeared in the third house. 6. The parts to be considered for the local wind forces were the edges of the walls, the edges of the x-direction of the roofs, and the locations of the width ratio of 0.4 of the first and third house and the center of the width of the second house for the y-direction of the roofs.

• 수산해양기술연구
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• 제38권1호
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• pp.43-57
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• 2002

본 연구는 고성능 전개판을 개발하기 위하여 전개판 주변의 유동장을 계측할 수 있는 해석 방법을 제시하고자 하였다. 실험 방법으로는 CFD를 이용한 유동장의 수치 해석과 유동장의 정량적, 정성적 계측이 가능한 PIV 실험방법을 사용하였다. 본 실험에서는 전개판 주변의 가시화된 영상을 PIV 기법을 이용한 화상처리로 유동특성을 해석하였으며, 이 결과를 CFD에 의한 해석 결과와 유동 패턴을 비교하였다. 또한, 회류 수조에서의 양력 계수 및 항력계수의 계측 결과를 상호 비교 하였다. 그 결과, 수치 해석된 결과와 PIV의 실험 결과는 정성적으로 매우 잘 일치하였으며, 물리적으로 타당성을 확인할 수 있었다. 그 결과는 다음과 같다. (1) 전개판의 유동장 분석을 위하여 레이저 광원을 이용한 가시화 실험을 실시하고, PIV 기법으로 화상분석을 실시하였으며, 유동입자의 흐름으로도 충분한 정성적인 유체운동의 경향을 파악할 수 있었다 (2) PIV해석결과가 정량적인 결과이므로 이를 다양한 후처리 방법을 통해 속도벡터장, 순간 유동장, 평균 와도로 나타내어 유동장의 변화를 확인할 수 있었다. (3) 최대전개력계수가 나타난 영각 24$^{\circ}$에서 비교한 CFD와 PIV 해석 결과, 유동 패턴은 유사하였고, 두 경우 모두 전개판 후연에서 약간의 경계층 박리가 발생하였으나 양호한 흐름을 보였다. (4) PIV에 의한 속도 벡터도, 순간 유선도, 평균 와도로 후처리한 결과, 영각 24$^{\circ}$에서부터 경계층 박리 현상이 일어나기 시작하여, 영각 28$^{\circ}$이상이 되면 심하게 전연으로 발생지점이 이동하게 되고, 그 폭도 확대됨을 확인할 수 있었다.

• Journal of Advanced Marine Engineering and Technology
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• 제31권7호
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• pp.842-851
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• 2007

Oscillating foil propulsion, the engineering application of fish-like movement of a hydrofoil, has received in recent decades as a possible competitor for propellers. The oscillating foil produces an effective angle of attack, resulting in a normal force vector with thrust and lift components, and it can be expected to be a new highly effective propulsion system. We have explored propulsion hydrodynamics as a concept in wake flow pattern. The present study has been examined various conditions such as oscillating frequencies and amplitudes in NACA0010 profile. Flow visualizations showed that high thrust was associated with the generation of moderately strong vortices, which subsequently combine with trailing-edge vorticity leading to the formation of a reverse $K\acute{a}rm\acute{a}n$ vortex street. Vortex generation was inherent to jet production and playeda fundamental role in the wake dynamics. And it was shown that the strong thrust coefficient obtained as the Strouhal number was larger.