• 한국추진공학회지
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• 제3권1호
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• pp.34-40
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• 1999

경사면에 충돌된 제트의 유동은 주제트(major jet)와 부제트(minor jet)로 나뉘어지게 되고 이로 인해 경사면 양쪽 영역에서의 유동 및 열전달 특성이 상이하게 된다. 또한 분사된 제트는 코안다 효과 (Coanda effect)로 인하여 경사면 위쪽으로 편향이 되어 충돌하게 된다. 이 결과 부제트영역에서 높은 난류 강도와 운동량를 얻을 수 있고, 국소 열전달계수를 상당히 높일 수 있다. 본 연구에서는 경사면의 각도와 분사속도를 변화시켰을 때 제트의 유동특성 변화 및 충돌면에서의 열전달 특성을 실험적으로 고찰하였다.

• 한국기계가공학회지
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• 제18권10호
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• pp.48-53
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• 2019

A water jet propeller is a key component that generates propulsion during the start of a naval vessel. When failure or breakage occurs, the vessel cannot operate. Recently, a flow analysis and structural analysis were conducted to understand the cause of damage to a bolt on a water jet. In particular, the stress and strain acting on the fastening bolt (impeller shaft and tail shaft) were examined to determine the extent of misalignment between the impeller shaft and the tail shaft of the water jet propeller. The study determined that stress and strain were concentrated on the impeller shaft and the tail shaft bolt. The alignment of the propeller impeller shaft and the tail shaft increased significantly in response to the tail shaft bolt. Failure of the tail shaft bolt fastening can lead to misalignment between the impeller shaft and the tail shaft.

• 한국터널지하공간학회 논문집
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• 제8권4호
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• pp.335-344
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• 2006

국내에서 제트팬 설치 간격 기준으로 사용되고 있는 일본도로공단 기준은 제트팬의 구경에 따라 설치간격을 제시하고 있지만 국제 상설도로 협회(PIARC)에서는 터널 직경에 10배를 유지할 것을 권장하고 있다. 이 기준들에 의해 결정된 설치 간격은 최대 약 2배 정도의 차이를 나타내고 있으며 이러한 설치 간격의 차이는 터널 환기 방식 선정에 불리한 요건으로 작용될 수 있기 때문에 터널 내부의 기류분석을 통한 적정 설치 간격 기준이 필요하다. 본 논문에서는 Froude 상사이론에 기초하여 아크릴 재질의 축소비 1/40의 모형 터널(직경 215mm, 연장 6.9m)과 모형 제트팬(구경 26.3mm, 31.6mm)을 제작하여 터널 내부에서의 기류분석을 위해 터널연장을 따라서 압력과 속도의 변화를 측정하였고, 제트팬 가동시 제트팬 주위에서 외부 공기의 영향으로 발생될 수 있는 재유입 현상을 확인하기 위해서 제트팬 주변에서 압력변화를 측정하였다. 모형실험 결과에서는 터널 내부기류는 제트팬 구경에 영향을 받지 않고 터널직경에 약 9배 정도가 되는 지점에서 압력과 속도의 변화가 안정되는 것으로 나타났으며 제트팬이 가동되면서 발생되는 재유입 현상을 확인할 수 있었다. 이러한 결과를 통해 터널 내부에서의 제트팬 설치 시에는 터널 직경에 약9배 이상을 확보해야 한다고 판단된다.

• 한국연소학회지
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• 제21권3호
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• pp.1-6
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• 2016

The effect of applied electric fields on jet flow instability was investigated experimentally by varying the direct current (DC) voltage and the alternating current (AC) frequency and voltage applied to a jet nozzle. We aimed to elucidate the origin of the occurrence of twin-lifted jet flames in laminar jet flow configuration, which occur when AC electric fields are applied. The results indicate that a twin-lifted jet flames originates from cold jet instability, caused by interactions between negative ions in the jet flow via electron attachment as $O_2+e{\rightarrow}O_2{^-}$ when AC electric fields are applied. This was confirmed by experiments in which a variety of gaseous jets were ejected from a nozzle to which DC voltages and AC frequencies and voltages were applied, with ambient air between two deflection plates connected to a DC power source. Experiments in which jet flows of several gases were ejected from a nozzle and AC electric fields were applied in coflow-nitrogen provided further evidence. The flow instability occurred only for oxygen and air jets. Additionally, jet instability occurred when the applied frequency was less than 80 Hz, corresponding to the characteristic collision response time. The effect of AC electric fields on the overall structure of the jet flows is also reported. Based on these results, we propose a mechanism to reduce jet flow instability when AC electric fields are applied to the nozzle.

• 대한기계학회논문집B
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• 제22권4호
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• pp.450-467
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• 1998

The characteristics of the unstable impinging circular jet is investigated based on the frequency characteristics and the sound field of the impinging-tones. Two symmetric modes S1 and S2, associated with low frequency and high frequency respectively, and one helical mode H have been observed. At low speed the S2 mode is dominant and switched by the S1 mode as the speed increases. When the jet speed is high the S1 mode is very active over the impinging distance from half the nozzle diameter to its ten times, while the S2 mode occurs at shorter distance corresponding to stage 2 and 3. The helical mode H seems unstable, likely to be influenced much by the experimental environment, and occurs at relatively high speed with almost the same frequency characteristics as the S2 mode. By estimating the convection speed of the unstable jet, it is found that the ratio of the convection speed to the jet speed decreases with both Strouhal number and Reynolds number and the speed of S2 mode is faster than the Si mode. When the present experimental results are compared with the previous investigations performed for the hole tone and the impinging tone with a small plate, the S1 mode is found to be associated with the ring vortex of large diameter with low speed, but the S2 mode with the vortex of small diameter with high speed. In addition, the frequency is found to be influenced by the nozzle configuration but the characteristics is almost the same. From the impinging distance and frequency range, it can be deduced that S1 mode is related with the jet column mode and S2 mode with the shear mode.

• Journal of Mechanical Science and Technology
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• 제15권12호
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• pp.1808-1815
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• 2001

The characteristics of a pulsed plasma jet originating from an electrothermal capillary discharge have been investigate using laser-induced fluorescence (LIF) measurement. Previous emission measurements of a 3.1 kJ plasma jet show trial upstream of the Mach disk the temperature and electron number density are about 14,000 K and and 10$\^$17/ cm$\^$-3/, while downstream of the Mach dick tole values are about 25,000 K and 10$\^$18/ cm$\^$-3/, respectively. However, these values are barred on line-of-sight integrated measurements that may be misleading. Hence, LIF is being used to provide both spatially and temporally resolved measurements. Our recent work has been directed at using planar laser-induced fluorescence (PLIF) imaging of atomic copper in the plasma jet flow field. Copper is a good candidate for PLIF studies because it is present throughout the plasma and has electronic transitions that provide an excellent pump-detect strategy. Our PLIF results to date show that emission measurements may give a misleading picture of the flow field, as there appeals to be a large amount of relatively low temperature copper outside the barrel shock. which may lead to errors in temperature inferred from emission spectroscopy. In this paper, the copper LIF image is presented and at the moment, relative density of atomic copper, which is distributed in the upstream of the pulsed plasma jet, is discussed qualitatively.

• 한국항공우주학회지
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• 제30권5호
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• pp.24-31
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• 2002

축 대칭 원형노즐 출구에 삼각형 형태의 작은 탭이나 얇은 테이프가 부착되었을 때 나타나는 초음속 제트유동장의 변화에 관한 연구가 쉴리렌 영상과 피토압력 측정을 통하여 수행되었다. 노즐 출구면적의 1 %에 해당하는 작은 탭에서 나타나는 유동방향 와류에 의한 제트유동 변화는 유동이 과소팽창 될 때 완전팽창과 과대팽창의 경우에 비하여 더 크게 나타나며 이로 인한 유동유입이 더 크게 나타남을 알 수 있었다. 탭의 설치각도 변화에 의한 영향도 평가되었으며, 유동이 과대팽창 될 때 노즐 안으로 구부러진 탭의 설치가 충격파의 간섭강도를 약화시키고 이로 인한 마하디스크의 소멸현상을 관찰할 수 있었다. 아울러 노즐내부 낮은 높이의 돌출부가 후방 유동장의 원주방향으로 압력변화를 나타내고, 이러한 압력변화는 유동의 팽창 정도에 영향을 받음을 알 수 있었다.

• 동력기계공학회지
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• 제18권4호
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• pp.23-28
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• 2014

In order to increase the performance of conventional hot water floor heating system, the bubble jet loop heat pipe for the system was developed. This experiment was conducted under next conditions : Working fluid was R-134a, charging ratio was 50%. A temperature of hot water, room temperature and flow rate were $60^{\circ}C$, $15^{\circ}C$ and 0.5~1.5 kg/min, respectively. The experimental results, show that bubble jet loop heat pipe had a high effective thermal conductivity of $4714kW/m^{\circ}C$ and a sufficient heat flux of $73W/m^2$ to heat the floor to $35^{\circ}C$ in case of the 1.5 kg/min of flow rate. So the bubble jet loop heat pipe has a possibility for appling of the floor heating system. Additionally, the visualization of bubble jet loop heat pipe was performed to understand the operating principle. Bubbles made by the narrow gap between inner tube and outer tube of evaporating part generate pulsation at liquid surface of working fluid. The pulsation had slug flow and wavy flow. So working fluid circulates in the bubble jet loop heat pipe as two phase flow pattern. And large amount of heat is transferred by the latent heat from evaporating part to condensing part.

• 대한기계학회논문집B
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• 제26권1호
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• pp.141-149
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• 2002

A numerical simulation is performed for the cooling heat transfer of a heated cylindrical pedestal by an axisymmetric jet impingement. Based on the k- $\varepsilon$- f$\sub$${\mu}$/ model of Park et at., the linear and nonlinear stress-strain relations are extended. The Reynolds number based on the jet diameter(D) is fixed at Re$\sub$D/ = 23000. The local heat transfer coefficients are compared with available experimental data. The predictions by k- $\varepsilon$-f$\sub$${\mu}$/ model are in good agreement with the experiments, whereas the standard 7- f model does not properly resolve the flow structures.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 추계학술대회논문집B
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• pp.260-267
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• 2001

The objective of this study was to investigate the characteristics of jet flow and heat transfer caused by trapezoid rods array in impinging jet system. In this study, trapezoid rods have been set up in front of flat plate to serve as a turbulence promoter. The bottom width of trapezoid rod was W=4, 8mm and oblique angle were $80^{\circ}$. The space from rods to the heating surface was C=1, 2, 4mm, the pitch between each rods was P=30, 40, 50mm, and the distance from nozzle exit to flat plate was H=100, 500mm. This results were compared with the case without trapezoid rods. As a result, when rods are installed in front of the impinging plate, the acceleration of the jet flow and the eddies due to the rods seem to contribute to the heat transfer enhancement. Among test conditions, the heat transfer performance was best for the condition of W=8mm, C=1mm, P=30mm and H/B=10. The maximum heat transfer rate is about 1.9 times larger than that without trapezoid rods.