• Journal of Advanced Marine Engineering and Technology
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• 제30권2호
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• pp.275-283
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• 2006

Experiment and three dimensional numerical investigations of incompressible turbulent flow through square channels with one- and two-sided ribbed walls are performed to determine pressure drop and heat transfer. The CFX(version 5.7) software package is used for the computation. The ribbed walls have a $45^{\circ}$ inclined square rib. Uniform heat flux is maintained on whole inner heat transfer channel area. The numerical results coincide with experimental data that obtained for $7,600{\le}Re{\le}24.900$, the pitch-to-rib height ratio (p/e) of 8.0. and the rib height-to-channel hydraulic diameter ratio ($e/D_h$) of 0.0667. The results show that values of local heat transfer coefficient and friction factor in the channel with two-sided ribbed wall are higher than those in the channel with one-sided ribbed walls.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2006년도 PARALLEL CFD 2006
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• pp.395-397
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• 2006

Air interlacing serves to protect the yarn against damage, strengthens inter-filament compactness or cohesion, and ensures fabric consistency. The air interlacing nozzle is used to introduce intermittent nips to a filament yarn so as to improve its performance in textile processing. The effect of various interlacing nozzle geometries on the interlacing process was studied. The geometries of interlacing nozzles with single or multiple air inlets located across the width of yarn channels are investigated. The basis case is the yarn channel, with a perpendicular main air inlet in the middle. Other cases have main air inlets, slightly inclined double sub air inlets, The yarn channel cross sectional shapes are either semicircular or rectangular shapes. The compressed impinging jet from the main air inlet hole hits the opposing bottom wall of the yarn channel, is divided into two branches, joins with the compressed air coming out from sub air inlet at the bottom and creates two free jets at both ends of the yarn channel. The compressed air movement in the cross-section consists of two opposing directional vortices. The CFD-FASTRAN flow parallel solver was used to perform steady simulations of impinging jet flow inside of the interlace nozzles. The vortical structure and the flow pattern such as pressure contour, particle traces, velocity vector plots inside of interlace nozzle geometry are discussed in this pater.

• 한국산학기술학회논문지
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• 제17권11호
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• pp.363-367
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• 2016

본 연구는 마하수 2.5의 초음속 영역에서 마하수 1.0의 슬롯 분사가 있는 후향계단 형상에 대한 유동장 특성을 분석하기 위하여 초음속풍동 시험부를 설계, 제작하였다. 비행체가 고속으로 움직일 때 공동 주위의 유동은 매우 복잡하여 수치해석 결과를 검증할 초음속풍동 시험 자료가 필요하기 때문에 기존의 2차원 대칭형 노즐을 아랫면이 평판인 비대칭형 노즐로 수정하였다. 특성곡선해법을 이용한 비점성 노즐을 설계하고, 시험을 통해 얻은 경계층 두께를 노즐에 반영하여 보정한 기법을 C 언어로 프로그래밍하여 얻은 결과를 수치해석 결과와 비교하여 검증하였다. 슬롯 분사 시 지속적인 유동장 변화 분석을 위한 초음속 유지시간 확보를 위해 저장탱크의 압력 변화에 따른 PID 제어프로그램 수정으로 초음속 유동 유지시간을 약 5초에서 약 6초로 1초 정도 연장하여 제어 효율을 향상하였고, 슬롯 분사가 있는 후향계단에서의 유동장 변화를 슐리렌장치로 가시화하여 복잡한 유동장 특성을 확인하였다. 향후 슬롯 분사의 속도와 유량, 유동장의 온도를 변화하여 공동에서의 막냉각 효과 분석을 위한 장비로 사용할 계획이다.

• 공업화학
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• 제33권1호
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• pp.96-102
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• 2022

고분자전해질막 연료전지의 반응물인 수소와 산소는 기체 상태이므로, 반응물이 원활히 전달될수록 작동 전압의 손실을 줄일 수 있다. 높은 전류밀도 영역에서 산소 물질 전달이 전압 손실을 좌우하므로, 환원극 유로의 형상 변경에 대한 연구들이 진행되어 왔다. 환원극 유로 형상 중에서 유로를 막는 블록은 반응물을 다공성 매질인 기체확산층으로 강제 대류 하도록 사용되었다. 본 연구에서는 간단한 단 채널의 연료전지 모델에 블록을 배치하였다. 전산 유체역학을 사용하였고, 공기 공급 유량을 달리하였을 때 블록으로 인한 강제 대류 효과가 전압-전류 곡선과 국부 전류 밀도에 대한 영향을 연구하였다. 기체확산층으로의 강제 대류 현상을 통하여 적은 공기 공급 유량으로도 높은 전류 밀도를 얻을 수 있었다. 다수의 블록을 직렬로 배치한 경우에 1개의 블록만 배치한 것보다 강제 대류 효과를 증가시켜 높은 전류밀도를 얻을 수 있었다.

• 한국항공우주학회지
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• 제34권12호
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• pp.48-58
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• 2006

횡단류에 분사되는 액체 제트의 분무 및 연소 특성에 대한 수치적 연구를 수행하였다. 수치 계산을 위해 3차원의 분무 및 화학반응 유동 해석에 유용한 KIVA 코드를 횡단류에서의 분무 해석에 적합하도록 수정하여 사용하였다. 액주의 분열과 리거먼트 및 액적의 분열 현상을 해석하기 위하여 wave 모델과 KH-RT hybrid 모델이 사용되었다. 침투길이는 유입공기의 속도가 감소하거나 분사속도가 증가함에 따라 증가하였다. 유입공기의 속도가 증가할수록 계산결과의 오차가 크게 발생함을 알 수 있었다. 연소 특성에 대한 수치 해석으로 연소실 내부의 화염전파 형상과 국부지역에서의 온도및 공해 배출량에 대한 결과를 얻었다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2003년도 제21회 추계학술대회 논문집
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• pp.271-277
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• 2003

최근 환경 소음이 사회적인 문제로 대두되고 있는 가운데, 생활수준의 향상으로 저소음화에 대한 요구가 증가되고 있는 실정이다. 이와 같이 소음에 관한 일반인들의 관심이 높아지면서 생환주변에서 주요 소음원으로 지적되고 있는 회전기계, 특히 가전제품을 비롯한 유동관련 기계류의 소음을 낮추기 위한 노력이 절실히 요구되고 있다. 본 소평팬에 대한 연구에서는 음압 및 음향인텐시티를 이용하여 소음원을 해석하였다. 이때, 광센서를 이용한 축류형 팬의 동기화가 수행되어졌고, 팬 형상에서 정확한 소음원의 위치를 규명하기 위한 기록시간의 결정이 제안되어졌다. 소음 발생하는 위치를 규명하였고, 지향성 연구를 통하여 축류형 팬의 방사형태를 결정하였으며, 음의 흐름도를 가시화 하였다.

• International Journal of Fluid Machinery and Systems
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• 제8권3호
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• pp.169-182
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• 2015

When simulating the dynamic behaviour of a hydro power plant, it is essential to have a good representation of the turbine behaviour. The pressure transients in the system occurs because the flow changes, which the turbine defines. The flow through the turbine is a function of the pressure, the speed of rotation and the wicket gate opening and is, most often described in a performance diagram or Hill diagram. In the Hill diagram, the efficiency is drawn like contour lines, hence the name. A turbines Hill diagram is obtained by performance tests on scaled model in a laboratory. However, system dynamic simulations have to be performed in the early stage of a project, before the turbine manufacturer has been chosen and the Hill diagram is known. Therefore one have to rely on diagrams for a turbine with similar speed number. The Hill diagram is drawn through measured points, so for using the diagram in a simulation program, one have to iterate in the diagram based on curve fitting of the measured points. This paper describes an alternative method. By means of the Euler turbine equation, it is possible to set up two differential equations which represents the turbine performance with good enough accuracy for the dynamic simulations. The only input is the turbine's main geometry, the runner blade in- and outlet angle and the guide vane angle at best efficiency point of operation (BEP). In the paper, simulated turbine characteristics for a high head Francis turbine, and for a reversible pump turbine are compared with laboratory measured characteristics.

• Journal of Advanced Marine Engineering and Technology
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• 제26권4호
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• pp.439-449
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• 2002

Experimental investigations of the flow structure and heat transfer enhancement in a channel with a built-in circular cylinder and a wing-let type vortex generator are presented. Without any vortex generators, relatively low heat transfer takes place in the downstream of the circular cylinder where is a recirculation region with low velocity fluid is formed. However with a wing-let type longitudinal vortex generator in the wake region behind the cylinder, heat transfer in the region can be enhanced. In order to control the strength of longitudinal vortices, the angle of attack of the vortex generators is varied from $20^{circ} to 45^{\circ}$, but spacings between the vortex generations are fixed to be 5 mm. The 3-dimensional mean velocity field downstream of the vortex generator is measured by a five-hole pressure probe, and the hue-capturing method using thermochromatic liquid crystals has been used to provide the local distribution of the heat transfer coefficient. The vorticity field and streamwise velocity contour are obtained from the velocity field. Streamwise distributions of averaged Stanton number on the measurement planes show very similar trends for all the experimental cases($\beta=20^{circ}, 30^{circ} and 45^{\circ}$). Circulation strength and heat transfer coefficient have the maximum values when the angle of attack($\beta$) is $30^{\circ}$.

• 한국실내디자인학회논문집
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• 제22권3호
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• pp.127-134
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• 2013

Baroque is fundamentally in contrast with renaissance style classicism, which attempted to fix a world view itself as the value of perpetuity. Furthermore, it is interpreted as a topic of incompletion or transformation that is not defined or is not exemplary and which may be enjoyed by people in the classical life, which requires a microscopic concept in contrast with dualism, the central axis of western civilization, namely, rational lucidity. Also, such characteristics are estimated to serve as a lubricant in life while going beyond the formal aesthetic level of art even from a contemporary perspective, and to play a productive role and to have potential. Consequently, this paper assumed that the concepts expressed by the 20th century US contemporary architect Richard Meier of a complex space, namely architectural formative vocabularies such as overlapping, interpenetration, collision, and collage style mixture created by a layered structure, in his architecture are in common with the double surface technique and juxtaposition of a flat structure of Baroque architecture. Then, the paper analyzed and considered the characteristics. The paper considered the following two issues: Such Baroque style formal principle is reinterpreted against a backdrop in which his architectural flow based on the domino theory of Le Corbusier became established as his own unique architectural feature, and it may be proposed as one big flow that enables us to seek again modernistic architecture that attempts to make an architectural space absolute as an atypical formal contour.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2005년도 제25회 추계학술대회논문집
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• pp.46-55
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• 2005

For the sea-level performance test of rocket motor designed to operate in the upper atmosphere, ejectors with no induced secondary flow are generally used, which serves dual purposes of evacuating the test cell and performing as a supersonic exhaust diffuser (SED). The main concern of this research is to simulate starting transients in order to visualize evolution of internal shock structures in SED with different initial cell (vacuum chamber) pressures. RANS code with low Reynolds $k-\varepsilon$ turbulence model was employed for these computations. Numerical results were compared with the pressure measurements previously performed [Proceedings of 2004 Annual Conference, KIMST], and showed good agreements with pressure-time history of measured data. In the case of low vacuum chamber pressure, abrupt impingement of the under-expanded supersonic jet from the nozzle onto the diffuser wall was observed, whereas initial impingement point was located downstream and moved slowly upstream in the case of non-vacuum chamber pressure. In spite of initially dissimilar evolution of shock structures, iso-mach contour revealed that the steady shock structures had little difference except the location of flow separation and normal shock.