• 한국산학기술학회논문지
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• 제20권2호
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• pp.655-661
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• 2019

본 연구는 차량용 리어 디퓨저의 시작 위치에 따른 주행 성능 변화를 분석하고자 하였다. 이를 위해 CATIA 3D 설계 프로그램을 이용하여 상용 SUV 차량을 참고하여 차량을 모델링하고 뒤 타이어를 기준으로 300, 400, 500 mm 떨어진 위치부터 리어 디퓨저가 시작되도록 설계했다. 그리고 유동 해석 프로그램인 Fluent를 이용해 차량 주행속도가 60km/h, 100km/h, 140km/h 일 경우를 조건으로 하여 유동해석 후 양력과 항력의 변화를 분석하고 공기의 유선 변화를 확인했다. 해석 결과, 리어 디퓨저는 시작 위치에 상관없이 디퓨저가 없는 경우에 비해 양력과 항력을 감소시켰다. 이는 리어 디퓨저가 있을 경우 공기가 차량 하면부를 지나 후면부로 빠져나올 때 발생하는 박리 현상을 억제하여 와류 현상을 감소시키기 때문이다. 또한 본 연구에서는 SP 400의 조건일 때 양력이 가장 작았고 양력 감소 효과도 가장 좋았기 때문에 주행 중 타이어의 접지력을 최대로 확보할 수 있어서 이 경우를 최적의 조건으로 결정하였다.

• 대한기계학회논문집B
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• 제23권10호
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• pp.1296-1309
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• 1999

A three dimensional compressible Navier-Stokes code is developed to analyze flowfields and performance of a vaned diffuser in a centrifugal compressor. It employs scalar implicit approximate factorization, finite volume formulation, second order upwind differencing and a two-equation $q-{\omega}$ turbulence model based on the integration to the wall. Pressure recovery and loss coefficients of a vaned diffuser are evaluated using a developed computer code. The simulated three dimensional flows show how through flow structure affects pressure recovery performance and loss coefficients of a vane for design and off-design inlet flow angles. Development of complex three dimensional flow over the inlet region and leading edge are very influential to the overall flow and performance.

• Journal of Advanced Marine Engineering and Technology
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• 제22권5호
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• pp.595-608
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• 1998

A diffuser an important equipment to change kinetic energy into pressure energy has been studied for a long time. Though experimental and theoretical researches habe been done the understanding of energy transfer and detailed mechanism of energy dissipation is unclear. As far as numerical prediction of diffuser flows are concerned various numerical studies have also been done. On the contrary many turbulence models have constraint to the applicability of diffuser-like flows with expansion and streamline curvature. In order to obtain the reliability of k-$\varepsilon$ turbulence model modified combination turbulence models composed of the anisotropic k-$\varepsilon$model modified combination turbulence models composed of the anisotropic k-$\varepsilon$ model with Hanjalic-Launder's preferential normal strain and Pope's vortex stretching mechanism are proposed. The results of the present proposed models prove the fact that the coefficient of pressure and the shear stress are well predicted at the diffuser flow.

• 한국생산제조학회지
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• 제24권4호
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• pp.394-399
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• 2015

Because flow uniformity affects the life cycle and performance of the catalyst, it is an important design factor for selective catalytic reduction (SCR) systems. We examined how the diffuser angle and the area ratio of the inlet of the SCR reactor to the front of the catalyst affect flow uniformity. For the numerical analysis, we used STAR-CCM+, a common CFD software program. Analysis results showed that the larger the area ratio was, the less the flow uniformity was, and that the longer the diffuser length was, the greater the flow uniformity was. When the area ratio was greater than 1:5, the flow uniformity appeared very similar at the front of the catalyst. As a result, the spread time of the exhaust gas increased and the flow velocity decreased.

• 대한기계학회논문집B
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• 제39권8호
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• pp.633-643
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• 2015

본 연구의 목적은 고효율 미세기포 공급장치인 산기관을 개발하기 위하여, 미세기포를 이용하여 하폐수에 용존산소를 효율적으로 공급하고 슬러지에 의한 기공의 막힘을 최소화함으로써 호기성 미생물에 의한 유기물 분해공정의 효율성과 내구성을 개선하고자 하였다. 종래의 미세기포 산기관을 개선하기 위하여, 실험과 전산해석 방법을 이용하여 미세기포를 발생시키면서 슬러지에 의한 막힘현상이 없는 원뿔형 산기관을 개발하였다. 전산해석을 통하여 단위 산기관 내부의 공기유동패턴을 확인하여 산기관 설계를 보완하고, 모의 생물반응기에 단위 산기관을 적용하여 발생 기포 거동 실험과 2상유체유동에 대한 전산해석을 수행하였다. 실험 결과로서 모의 생물반응기 내에서 발생기포 수직 길이 및 상승속도 등 기포거동에 대한 통계치를 도출하였으며, 전산해석 결과로서 기포군의 거동을 포함한 유동특성에 대한 메커니즘을 규명하였다. 이를 통하여 고효율 산기관 설계를 체계화하였고 모의 생물반응기 내에서 기포거동과 내부유동 현상을 규명함으로써, 실증 수처리장 규모 생물반응기에 산기관 군체를 적용하여 산소전달특성 및 내부유동특성을 파악하고 시스템을 설계하는데 중요한 근거를 제시하였다.

• 소음진동
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• 제4권3호
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• pp.377-384
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• 1994

This paper is an investigation of the performance of absorption diffusers to suppress the vent noise emitted when high pressure gas is throttled. First, experiment for the static performance is carried out. When there is no through-flow, the insertion loss has been obtained in terms of 1/3 octave band spectrum and the effect of the number of diffusers and the thickness of the absorption material on the static performance has been obtained. And the similarity in the spectrum of the static insertion loss is confirmed by comparing two similar models with different size. Second, the dynamic performance has been obtained by experiment using blow-down of compressed air from a storage tank through an orifice of diameter 10 mm. The back pressure by the diffuser is measured and compared with that of a single diffuser. It is found that the insertion loss of asingle diffuser is very low around 3 dB at high frequencies with negative value at low frequencies. By absorption material between the diffuser tubes, however, the performance is increased considerably. Without flow the static insertion loss increases by 3 - 4 dB by doubling the thickness or the density of the absorptionmaterial. With flow, however, the dynamic insertion loss increases. While, the back pressure by the diffuser is small enough to be neglected.

• 한국유체기계학회 논문집
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• 제11권2호
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• pp.55-63
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• 2008

An examination of the condition of the flow leaving the impeller exit kinetic energy often accounts for 30-50% of the shaft work input to the compressor stage, and for energy efficiency it is important to recover as much of this as possible. This is the function of the diffuser which follows the impeller. The purpose of this study is to investigate the sensitivity of how compressor performances changes as vaned diffuser geometry is varied. Three kinds of vaned diffusers were studied and its results were compared. First vaned diffuser type is based on NACA airfoil and second is channel diffuser and third is conformal transformation of NACA65(4A10)06 airfoil. Mean-line prediction method was applied to investigate the performance and stability for three kinds of diffusers. And CFD analyses have been done for comparison and detailed interior flow pattern study. NACA65(4A10)06 airfoil showed the widest operating range and higher pressure characteristics than the others.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제37회 추계학술대회논문집
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• pp.182-186
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• 2011

Ejector-diffuser system has long been used in many diverse fields of engineering applications and it has advantages over other fluid machinery, because of no moving parts and structural simplicity. This system makes use of high-pressure primary stream to entrain the low-pressure secondary stream through pure shear actions between two streams. In general, the flow field in the ejector-diffuser system is highly complicated due to turbulent mixing, compressibility effects and sometimes flow unsteadiness. A fatal drawback of the ejector system is in its low efficiency. Many works have been done to improve the performance of the ejector system, but not yet satisfactory, compared with that of other fluid machinery. In the present study, a mixing guide vane was installed at the inlet of the secondary stream for the purpose of the performance improvement of the ejector system. A CFD method has been applied to simulate the supersonic flows inside the ejector-diffuser system. The present results obtained were validated with existing experimental data. The mixing guide vane effects are discussed in terms of the entrainment ratio, total pressure loss as well as pressure recovery.

• 한국추진공학회지
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• 제9권2호
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• pp.70-77
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• 2005

축소-팽창 디퓨저가 장착된 초음속 이젝터를 제작하여, 다양한 위치에서의 측정된 압력으로 부유동의 초음속 시동조건을 찾아내었다. 우선 부유동 흡입구의 크기의 영향을 알아내기 위하여 다양한 흡입구 직경으로 실험하였으며, 부유동의 초음속 시동은 흡입구 직경과 축소-팽창 디퓨저 직경의 비, d/D가 0.306 미만인 경우에만 일어났다. 이보다 큰 d/D에서는, 아음속 시동이 먼저 시작되고, 흡입구를 막으면서 주유동의 유입이 전 유동장을 채우게 되어 수직 충격파를 축소-팽창 디퓨저의 하류로 내려보내게 된다 이러한 상황에서 다시 흡입구를 열어도 히스테리시스의 영향으로 초음속 시동이 유지된다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2005년도 창립60주년 기념 추계 학술대회
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• pp.83.2-83.2
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• 2005