• 한국유체기계학회 논문집
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• 제18권5호
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• pp.49-53
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• 2015

Thrust vector control is the method which generates the side force and roll moment by controlling exhausted gas directly in a rocket nozzle. TVC is classified by mechanical and fluid dynamic methods. Mechanical methods can change the flow direction by several objects installed in a rocket nozzle exhaust such as tapered ramp tabs and jet vane. Fluid dynamic methods control the flight direction with the injection of secondary gaseous flows into the rocket nozzle. The tapered ramp tabs of mechanical methods are used in this paper. They installed at the rear in the rocket nozzle could be freely moved along axial and radial direction on the mounting ring to provide the mass flow rate which is injected from the rocket nozzle. TVC of the tapered ramp tabs has the potential to produce both large axial thrust and high lateral force. We have conducted the experimental research and flow analysis of ramp tabs to show the performance and the structural integrity of the TVC. The experiments are carried out with the supersonic cold flow system and the schlieren graph. This paper provides to analyze the location of normal shock wave and distribution of surface pressure on the region enclosed by the tapered ramp tabs.

• Journal of Mechanical Science and Technology
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• 제14권2호
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• pp.226-235
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• 2000

The performance prediction of an airfoil fan using a commerical code, STAR/CD, is verified by comparing the calculated results with measured performance data and velocity fields of an airfoil fan. The effects of inlet tip clearance on performance are investigated. The calculations overestimate the pressure rise performance by about 10-25 percent. However, the performance reduction due to tip clearance is well predicted by numerical simulations. Main source of performance decrease is not only the slip factor but also impeller efficiency. The reduction in performance is 12-16 percent for 1 percent gap of the diameter. The calculated reductions in impeller efficiency and slip factor are also linearly proportional to the gap size. The span-wise distributions of phase averaged velocity and pressure at the impeller exit are strongly influenced by the radial gap size. The radial component of velocity and the flow angle increase over the passsage as the gap increases. The slip factor decreases and the loss increases with the gap size. The high velocity of leakage jet affects the impeller inlet and passage flows. With a larger clearance, the main stream moves to the impeller hub side and high loss region extends from the shroud to the hub.

• 한국해안해양공학회지
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• 제13권2호
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• pp.109-121
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• 2001

잠재된 평판 방파제가 해수 교환에 미치는 영향을 실험적으로 조사하였고 그 결과를 제시한다. 흐름은 PIV 시스템으로 관측되었으며 조화분석으로부터 분리된 평균 흐름과 파랑 타원이 각각 제시된다. 실험결과, 순환유량은 입사파의 체적플럭스와 밀접한 관계가 있으며 쌍와류가 평판 후면에서 관측되었다. 염료추적에 의하면 평판위에서 발생된 제트류로 인한 난류의 영향으로 유입되는 해수와 항내 오염물질이 상당히 잘 섞이고 있음을 보여주고 있다.

• 물과 미래
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• 제27권2호
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• pp.63-72
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• 1994

본 연구에서는 단계식어도 내의 격벽 형상, 잠공설치, 측벽 홈설치 등에 따른 수리현상을 수리시험을 통해 규명하고 어족의 소상에 적합한 적정 구조물 형상을 제시함으로써 어도 구조물 설계에 지침이 되도록 하였다. 분석 결과 어족의 소상은 표면류 상태가 바람직하며, 잠공설치는 어족 소상을 방해하는 것으로 나타났다. 또한 측벽에 설치된 홈을 돌출부로 대치함으로써 격벽 월류 유속을 줄이고 소상을 용이하도록 했으며, 퇴적된 토사를 제거하기 위해 고정식 격벽보다는 상·하 2단식 수직이동 격벽을 설치하며, 새들에 의한 어족의 피해를 고려하여 그물망을 설치하고, 어도 바닥의 색깔을 통과 어족의 색깔과 같이 함으로써 보호색 기능을 갖추는 것이 바람직한 것으로 판명되었다.

• 한국농공학회지
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• 제34권E호
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• pp.30-44
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• 1992

A modification of the TEACH-like computer program based on the k-$\varepsilon$ turbulence transport was applied for predicting air mixing patterns and temperature distributions in a rectangular, slot-ventilated enclosure having obstructions ; a rectangular obstacle with heat flux, solid walls separates the passage and the pig pens, and purlins beneath the ceiling. Air flow patterns were calculated for the cases with and without the purlin, extending 300mm beneath the ceiling. Comparisons of prediction data of Randall & Battams(1976) showed air flow pattern predicted well for the case without the purlin. Heat was accumulated at the corner of the left side of the solid wall and the right-upper region of the simulated pigs. However the air distribution pattern was completely different from data for the case with the purlin. The deviation from the observation may be attributed to the difference of the geometric configuation. Exploring the cause of the deviation should be conducted in a further study. Temperature stratification was also observed due to incomplete mixing. The obstruction in the route of the inlet air jet at inlet should be avoided since most of kinetic energy dissipates at the abstacle duet to impingement.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.358-363
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• 2008

The spray cross-section characteristics of two-phase spray that using external-mixing nozzle injected into a subsonic cross flow were experimentally studied with various ALR ratio that is $0{\sim}59.4%$. Suction type wind tunnel was used and experiments were conducted to ambient environment. Several plain orifice nozzles with L/d of 30 and orifice diameter of 0.5 mm and orifice length 1.5 mm were tested. Free stream velocity profiles at the injection location were measured using hot wire. Spray images were captured to study collision point and column trajectory. Phase Doppler particle analyzer(PDPA) was utilized to quantitatively measuring droplet SMD, volume flux. Measuring probe of PDPA positions was moved 3-way transverse machine. SMD distributions were layered structure and peaked at the top of the spray plume and low value at bottom of the spray. Volume flux of spray was distributed to the two side region and volume flux quantity decreased when ALR ratio increased. It was found that the perpendicularly injected two-phase spray jet of external mixing into a cross flow showing that mistlike spray moved away from the test section bottom region.

• 한국지열·수열에너지학회논문집
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• 제15권3호
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• pp.7-13
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• 2019

To improve the flow distribution at channel locations in the welded plate heat exchanger with "L"-type inflow, the flow visualization of Model 1 was carried out. Besides, the characteristics of flow distribution was investigated experimentally according to the header shape. The inlet flow rate for each channel location was increased at the side channels but decreased at the central channels. In the case of Model 2, which has a slant structure added to the basic header of Model 1, the unevenness of inlet flow increased by 23% from 0.019 to 0.023 as compared to Model 1. On the other hand, Model 3, which has a baffle structure added to Model 2, showed 0.064 unevenness in inlet flow, which was a 36% reduction one compared to Model 1. To improve the distribution at each channel in the welded plate heat exchanger with "L"-type flow, it is necessary to improve the header external shape for the guide of flow as well as the baffle structure for reduction of vortex flow.

• Maxillofacial Plastic and Reconstructive Surgery
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• 제18권4호
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• pp.570-593
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• 1996

본교실에서 하악지 시상 골절단술을 시행한 하악전돌증 환자 20명(남자 9명, 여자 11명)을 대상으로 술전, 술직후, 장기관찰기간동안의 전산화단층촬영법을 이용한 하악과두의 위치변화와 술전, 술직후, 악간고정제거 24시간후 및 장기관찰기간동안의 측모두부방사선사진에서의 재발과의 상관관계를 연구한 결과 다음과 같은 결과를 얻었다. 1. 두부 축방향 전산화단층사진에서의 과두간거리(MM')는 $84.45{\pm}4.01mm$ 였으며, 장축각은 우측 11.89%5.1 $9^{\circ}$좌측 $11.65{\pm}2.09^{\circ}$로 좌우 비슷하였으며, 기준선(AA')에서 과두의 외측점은 12mm, 내측점은 7mm 정도 전방에 위치하였다. 관상면 전산화단층사진에서의 과두간 거리(mm')는 $84.43{\pm}3.96mm$ 였으며, 사축각은 우측 $78.12{\pm}3.43^{\circ}$ 좌측 $78.09{\pm}6.12^{\circ}$로 좌우 비슷하였다 . 2. 술전후 과두위치 변화(T2C-T1C)는 통계적인 유의성은 없었으나(p>0.05), 다소 증가하는 경향을 보였으며, 장기관찰에 따른 회귀성향(TLC-T2C)에서는 LMD, LLD(p<0.05), RLD, RMD(p<0.01), mm'(P<0.001)는 모두 감소하였다. 3. 측면두부방사선사진상에서 술직후와 악간고정제거 24시간후(T3-T2)에서 하악의 초기재발은 통계적인 의의가 없었으며(p>0.05) 하악전치의 경우만 평균 0.33mm 전방이동하였다(p<0.05). NN'L1, NN'Pog, NN'Gn, NN'Me, over-jet에서 통계적인 유의성이 있었으며(p<0.05), NN'Ll 1.2%, NN'B 5.0%, NN'Pog 2.0%, NN'Gn 9.1%, NN'Me 10.3%의 총재발량을 보였다. 4. 하악골의 술전, 술후 변화량(T2-T1)이 총재발량에 미치는 영향에 대한 회귀분석에서 후퇴량이 많을수록 하악골의 총재발량이 많은 것으로 나타났다(p<0.05). 5. 하악골 변화량(T2-T1)과 하악과두 변화량(T2C-T1C, TLC-T2C), 하악과두 변화량(T2C-T1C, TLC-T2C)과 총재발량(TL-T2), 술전 하악과두 형태(T1C)와 하악과두 변화량(T2C-T1C, TLC-T2C), 그리고 술전 하악골 외형(T1)과 하악과두 변화량(T2C-T1C, TLC-T2C)에 대하여 단순 및 복잡회귀분석에서 통계적인 유의성은 없었다(p>0.05). 6. 술전 하악과두 형태(T1C)가 총재발량(TL-T2)에 미치는 영향에 대한 복잡회귀분석결과 우측과두에서는 과두간 거리가 멀고 장축각이 적고 사축각이 클수록 하악골의 수평적인 재발(NN'Ll, NN'8, NN'Pog, NN'Gn, NN'Me)이 많은 것으로 나타났으며(p<0.05), 좌측과두에서는 NN'Ll, NN'Me에서 같은 결과를 보였다. 7, 술전 하악과두 형태(T1C)가 술전 하악골외형(T1)에 미치는 영향에 대한 복잡회귀분석결과 우측과두에서는 과두간 거리가 멀고 장축각이 적고 사축각이 클수록 하악골의 수직고경이 큰 것으로 나타났고(p<0.05), 좌측과두에서는 과두간 거리가 멀고 장축각이 적고 사축각이 클수록 수직고경이 크며, 전돌된 양상으로 나타났다(p<0.05) . 8. 술전 하악골 외형(T1)이 총 재발량(TL-T2)에 미치는 영향에 대하여 단순회귀분석을 시행한 결과 NN'L1, NN'B, NN'Gn, NN'Me, over-jet 둥의 계측점에서 하악골이 전돌된 양상을 보일수록 NN'B에서의 총재발량은 많은 것으로 나타났다(p<0.05). 또 수평피개량(over-jet)이 클수록 NN'B, NN'Pog, NN'Gn, NN'Me에서의 총재발량이 많은 것으로 나타났다(p<0.05). 따라서 과두보존술을 이용하여 과두를 안정화시키고 난후 악골 형태를 재구성하였을 때 이로 인하여 생기는 하악과두 이동은 미미하여 술후 재발에 크게 영향을 미칠 정도는 아니라고 사료된다.

• 한국지구과학회지
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• 제31권4호
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• pp.354-369
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• 2010

2006년 10월 22일에서 24일에 걸쳐 한반도 강릉지역에서 강한 집중호우가 발생했다. 이 기간에 대해서 집중호우가 발생하기 전과 강우강도가 가장 강했을 때 나타나는 종관적, 운동학적 특성을 조사하기 위하여 본 연구에서는 지상일기도, 상층일기도, 적외위성영상, 자동기상관측장비(AWS) 자료, NCEP(National Centers for Environmental Prediction) 전구분석자료를 이용하였다. 분석 기간 동안 강릉에서 관측된 총 강수량은 316.5 mm이고, 최대 순간풍속은 $63.7m\;s^{-1}$이다. 일기도를 분석해보면 집중호우가 시작하기 전 온대저기압이 한반도 중부에서 발달하였으며 한반도 북부에 역전기압골이 형성되어 있다. 또한 300 hPa 상층일기도에서는 서해와 한반도 남부에 제트기류가 위치하며, 위치 소용돌이도 이상과 관련된 절리 저기압이 한반도 북서부에서 발달하고 있다. 강우강도가 가장 강했을 때의 특성을 좀 더 자세히 알아보기 위하여 강릉지역의 위치 소용돌이도 이상과 바람, 위치 소용돌이도의 시간-연직 단면도, 연직운동, 발산장과 수렴장, 역학적 온위의 연직분포에 대해 조사하였다. 종관적, 운동학적 과정을 분석해 본 결과 대류권계면 접힘이 집중호우 발생에 큰 역할을 한 것으로 사료된다.

• Wind and Structures
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• 제35권1호
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• pp.1-20
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• 2022

This research work presents an experimental study's outcomes to reveal the impact of an O-ring on the flow control over a sphere placed in a turbulent boundary layer. The investigation is performed quantitatively and qualitatively using particle image velocimetry (PIV) and dye visualization. The sphere model having a diamater of 42.5 mm is located in a turbulent boundary layer flow over a smooth plate for gap ratios of 0≤G/D≤1.5 at Reynolds number of 5 × 10³. Flow characteristics, including patterns of instantaneous vorticity, streaklines, time-averaged streamlines, velocity vectors, velocity fluctuations, Reynolds stress correlations, and turbulence kinetic energy (), are compared and discussed for a naked sphere and spheres having O-rings. The boundary layer velocity gradient and proximity of the sphere to the flat plate profoundly influence the flow dynamics. At proximity ratios of G/D=0.1 and 0.25, a wall jet is formed between lower side of the sphere and flat plate, and velocity fluctuations increase in regions close to the wall. At G/D=0.25, the jet flow also induces local flow separations on the flat plate. At higher proximity ratios, the velocity gradient of the boundary layer causes asymmetries in the mean flow characteristics and turbulence values in the wake region. It is observed that the O-ring with various placement angles (𝜃) on the sphere has a considerable alteration in the flow structure and turbulence statistics on the wake. At lower placement angles, where the O-ring is closer to the forward stagnation point of the sphere, the flow control performance of the O-ring is limited; however, its impact on the flow separation becomes pronounced as it is moved away from the forward stagnation point. At G/D=1.50 for O-ring diameters of 4.7 (2 mm) and 7 (3 mm) percent of the sphere diameter, the -ring exhibits remarkable flow control at 𝜃=50° and 𝜃=55° before laminar flow separation occurrence on the sphere surface, respectively. This conclusion is yielded from narrowed wakes and reductions in turbulence statistics compared to the naked sphere model. The O-ring with a diameter of 3 mm and placement angle of 50° exhibits the most effective flow control. It decreases, in sequence, streamwise velocity fluctuations and length of wake recovery region by 45% and 40%, respectively, which can be evaluated as source of decrement in drag force.