• 한국유체기계학회 논문집
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• 제10권6호
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• pp.17-23
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• 2007

In the present work, flow analysis has been performed in the steam turbine bypass control valve (single-path type) for two different cases i.e., case with steam only and case with both steam and water. The numerical analysis is performed by solving three-dimensional Reynolds-averaged Navier-Stokes (RANS) equations. The shear stress transport (SST) model and $k-{\varepsilon}$ model are used to each different case as turbulence closure. Symmetry condition is applied at the mid plane of the valve while adiabatic condition is used at the outer wall of the cage. Grid independency test is performed to find the optimal number of grid points. The pressure and temperature distributions on the outer wall of the cage are analyzed. The mass flow rate at maximum plug opening condition is compared with the designed mass flow rate. The numerical analysis of multiphase mixing flow(liquid and vapor) is also performed to inspect liquid-vapor volume fraction of bypass valve. The result of volume fraction is useful to estimate both the safety and confidence of valve design.

• 한국습지학회지
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• 제14권4호
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• pp.439-455
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• 2012

파랑 수치모형인 SWAN 수치모형, 파랑에 의해 발생되는 기인력 수치모형인 WIF 수치모형, 그리고 흐름장 수치모형은 EFDC 수치모형을 연동하여 최종적으로 파랑류 계산이 가능한 WIC 수치모형을 개발하였다. 개발된 WIC 수치모형을 검증하기 위하여 Goda(2000)가 적용한 수중 원형천퇴의 파랑변형 계산하여 파고, 파랑의 굴절과 회절을 비교하였으며, 파고비 결과는 약 1~5 %의 차이를 보였다. 파랑에 의한 기인력 수치모형은 기존의 Longuet-Higgins and Stewart(1960)가 제안한 잉여응력에 의해 발생하는 기인력에 Dally and Osiecki(1994)가 제안한 roller로 인한 응력에 의해 발생되는 기인력을 추가하였고, Kim(2004)이 제안한 완화기법을 도입하여 lateral mixing 처리를 수행하지 않아도 자연현상과 유사한 결과를 얻을 수 있도록 개발되었다. 개발된 파랑에 의한 기인력 수치모형은 계산시 ${\Delta}t$에 제약을 받지 않는다는 장점을 가지고 있으며, 흐름장 수치모형의 source항이 되어 파랑류의 양상을 계산할 수 있도록 하였다. 연계된 파랑류 수치모형을 검증하기 위해서 Nishimura et al.(1985)의 수리모형실험과 Kim(2004)의 수심적분된 파랑류 수치모형과 비교하였다. 이안제 배후에서 연안류의 유속분포와 이안류의 유속분포 결과가 기존의 수리모형실험과 수치모형실험의 결과와 상당히 일치함이 관측되었다.

• Smart Structures and Systems
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• 제4권1호
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• pp.67-84
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• 2008

The present contribution is concerned with the static and dynamic stability of a piezo-laminated Bernoulli-Euler beam subjected to an axial compressive force. Recently, an inconsistent derivation of the equations of motions of such a smart structural system has been presented in the literature, where it has been claimed, that an axial piezoelectric actuation can be used to control its stability. The main scope of the present paper is to show that this unfortunately is impossible. We present a consistent theory for composite beams in plane bending. Using an exact description of the kinematics of the beam axis, together with the Bernoulli-Euler assumptions, we obtain a single-layer theory capable of taking into account the effects of piezoelectric actuation and buckling. The assumption of an inextensible beam axis, which is frequently used in the literature, is discussed afterwards. We show that the cited inconsistent beam model is due to inadmissible mixing of the assumptions of an inextensible beam axis and a vanishing axial displacement, leading to the erroneous result that the stability might be enhanced by an axial piezoelectric actuation. Our analytical formulations for simply supported Bernoulli-Euler type beams are verified by means of three-dimensional finite element computations performed with ABAQUS.

• 대한조선학회논문집
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• 제41권6호
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• pp.24-32
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• 2004

The effects of guide vanes and tip clearances on the characteristics nf axial flow fans are investigated both computationally and experimentally. Performance test of fans carried out in full scale shows considerable effects of tip clearance between rotor tip and duct on the characteristics of fans. The tested results are compared with the computation based on the finite volume method to solve the Navier-Stoke equations with $textsc{k}$-$\varepsilon$ turbulence model. The comparison shows good agreements between experimental and computational results. In addition, the effects of shape of guide vanes are numerically studied. The results show that increased volume of separated region around the guide vane reduces the recovery of tangential component of kinetic energy in the wake, resulting in loss of efficiency

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.150-156
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• 2008

A program based on a 2-D CFD code has been developed to simulate a gas turbine engine. 2-D Navier-Stokes implicit code with $k-\omega$ turbulent model is used in compressor and turbine. Lumped method chemical equilibrium code with 10 species of molecular is applied to combustor with assuming perfect mixture and 100% combustion efficiency at constant pressure state. Fluid properties are shared on interfaces between engine components. Compressor supplies outlet temperature and pressure to combustor. At the same time, combustor also carries temperature and pressure to turbine. The back pressure of compressor outlet is transferred by inlet pressure of turbine. Unsteady phenomena in rotor-stator are covered by mixing-plane method. The running condition of engine can be determined only by given the inlet condition of compressor, the outlet condition of turbine, equivalence ratio and rotating speed.

• Geomechanics and Engineering
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• 제34권5호
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• pp.491-505
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• 2023

The practical usage of underground space and demand for vehicular tunnels necessitate the construction of non-circular wide rectangular tunnels. However, constructing large tunnels in soft clayey soil conditions with no ground improvement can lead to excessive ground deformations and collapse. In recent years, in situ ground improvement techniques such as jet grouting and deep cement mixing are often utilized to perform cement-stabilisation around the tunnel boundary to prevent large deformations and failure. This paper discusses the stability characteristics and failure behaviour of a wide rectangular tunnel in cement-treated soft clays. First, the plane strain finite element model is developed and validated with the results of centrifuge model tests available in the past literature. The critical tunnel support pressures computed from the numerical study are found to be in good agreement with those of centrifuge model tests. The influence of varying strength and thickness of improved soil surround, and cover depth are studied on the stability and failure modes of a rectangular tunnel. It is observed that the failure behaviour of the tunnel in improved soil surround depends on the ratio of the strength of improved soil surround to the strength of surrounding soil, i.e., q_ui/q_us, rather than just q_ui. For low q_ui/q_us ratios,the stability increases with the cover; however, for the high strength improved soil surrounds with q_ui >> q_us, the stability decreases with the cover. The failure chart, modified stability equation, and stability chart are also proposed as preliminary design guidelines for constructing rectangular tunnels in the improved soil surrounded by soft clays.

• Restorative Dentistry and Endodontics
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• 제18권1호
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• pp.1-26
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• 1993

The purpose of this study was to investigate the effect of acid etching on the surface appearance and fracture toughness of five glass ionomer cements. Five kinds of commercially available glass ionomer cements including chemical curing filling type, chemical curing lining type, chemical curing metal reinforced type, light curing tilling type and light curing lining type were used for this study. The specimens for SEM study were fabricated by treating each glass ionomer cement with either visible light curing or self curing after being inserted into a rubber mold (diameter 4mm, depth 1mm). Some of the specimens were etched with 37% phosphoric acid for 0, 15, 30, 60, go seconds, at 5 minutes, 1 hour and 1 day after mixing of powder and liquid. Unetched ones comprised the control group and the others were the experimental groups. The surface texture was examined by using scanning electron microscope at 20 kV. (S-2300, Hitachi Co., Japan). The specimens for fracture toughness were fabricated by curing of each glass ionomer cement previously inserted into a metal mold for the single edge notch specimen according to the ASTME399. They were subjected to a three-point bend test after etching for 0, 30, 60, and 90 seconds at 5 minutes-, 1 hour-and 1 day-lapse after the fabrication of the specimens. The plane strain fracture toughness ($K_{IC}$) was determined by three-point bend test which was conducted with cross-head speed of 0.5 mm/min using Instron universal testing machine (Model No. 1122) following seven days storage of the etched specimens under $37^{\circ}C$, 100% humidity condition. Following conclusions were drawn. 1. In unetched control group, crack was present, but the surface was generally smooth. 2. Deterioration of the surface appearance such as serious dissolving of gel matrix and loss of glass particles occured as the etching time was increased beyond 15 s following Immediate etching of chemical curing type of glass ionomer cements. 3. Etching after 1 h, and 1 d reduced surface damage, 15 s, and 30s etch gave rough surface appearance without loss of glass particle of chemical curing type of glass ionomer cements. 4. Light curing type glass ionomer cement was etched by acid, but there was no difference in surface appearances according to various waiting periods. 5. It was found that the value of plane stram fracture toughness of glass ionomer cements was highest in the light curing filling type as $1.79\;MNm^{-1.5}$ followed by the light curing lining type, chemical curing metal reinforced type, chemical curing filling type and chemical curing lining type. 6. The value of plane stram fracture toughness of the chemical curing lining type glass ionomer cement etched after 5 minutes was lower than those of the cement etched after 1 hour or day or unetched (P < 0.05). 7. Light curing glass ionomer cement showed Irregular fractured surface and chemical curing cement showed smooth fractured surface.

• 대한기계학회논문집B
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• 제27권4호
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• pp.466-475
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• 2003

The gun-type gas burner adopted in this study is generally composed of eight slits and swirl vanes. Thus, this paper is studied to investigate the effect of slits and swirl vanes on the turbulent flow fields in the horizontal plane of gas swirl burner with a cone type baffle plate measured by using X-probe from hot-wire anemometer system. This experiment is carried out at flow rate 450 $\ell$/min in the test section of subsonic wind tunnel. The axial mean velocity component in the case of burner model with only swirl vanes shows the characteristic that spreads more remarkably toward the radial direction than axial one, it does, however, directly opposite tendency in the case of burner model with only slits. Consequently. both slits and swirl vanes composing of gun-type gas burner play an important role in decrease of the speed near slits and increase of the flow speed in the central part of a burner because the biggest speed spurted from slits encircles rotational flow by swirl vanes and it drives main flow toward the axial direction. Moreover, the turbulent intensities and turbulent kinetic energy of gun-type gas burner are distributed with a fairly bigger size within X/R<0.6410 than burner models which have only slits or swirl vanes because the rotational flow by swirl vanes and the fast jet flow by slits increase flow mixing, diffusion, and mean velocity gradient effectively.

• 플랜트 저널
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• 제18권2호
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• pp.41-45
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• 2022

머드 유동 압력파를 이용한 기존의 통신방식은 속도가 1-2 bps 수준으로서 통신에 소요되는 시간이 길어 실시간 제어가 불가능한 수준이다. 통신 속도를 10배 이상 향상시키기 위한 음파통신 방식은 상용화되기는 하였으나 가격이 비싸 이용이 제한적이고 응용 사례도 많지 않다. 본 연구는 해당 설비에 해당하는 시뮬레이터를 개발하여 실제 시험 결과와 유사하게 성능을 개발하였다. 드릴 파이프를 통한 음파 통신 모사를 위해 머드에 의한 마찰 감쇠를 모사할 수 있는 지배 방정식을 제안하고 수치해석 모델을 개발하였다. 감쇠 계수는 시추 현장에서의 음파 에너지 감쇠율과 비교하여 보정하였다. 개발된 수치해석 모델을 대상 QPSK 변조 방식의 통신 알고리즘을 적용하여 지상부에서 통신 에러율 0.04% 수준의 우수한 성능을 확인하였다. 이는 아직 노이즈가 혼입되지 않은 조건에서의 통신 성능이며 이를 적용하기 위해 현장 노이즈 데이터를 확보하여 혼입을 위한 실제 노이즈 신호를 재생하는 기술을 확립하였다.

• 대한기계학회논문집
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• 제16권8호
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• pp.1552-1565
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• 1992

본 연구에서는 공기와 연료의 혼합을 원활하게 함으로써 완전연소가 가능하도 록 하기 위하여 이용되는 스월 및 스쿼시 유동이 연소실 내부유동장 변화에 미치는 영 향을 조사하기 위하여 흡입행정 및 연료분무 직전까지의 압축행정에 대해 연소실 내부 유동장을 수치해석하고자 한다.수치해석에는 EPISO-SPRAY 코드를 수정, 보완하여 이용했는데 이 코드는 미국 Los Alamos 연구소를 중심으로 개발된 CONCHAS 계열이나 KIVA 계열의 코드와는 달리 밸브의 개폐운동을 처리할수 있도록 구성되어 있다. 난류모델은 피스톤의 압축 및 팽창에 따른 밀도변화를 고려하여 수정한 k-.epsilon. 모델을 이용한다. 계산은 편심밸브를 갖는 두가지 연소실 형상, 즉 피스톤 보울이 없는 경 우와 피스톤 보울이 있는 경우의 연소실에 대해 선회비를 변화시키며 ATDC 0도부터 ATDC 340도까지의 연료분무가 없는 경우의 3차원 유동장 해석을 통해 흡입 공기가 갖 는 스월과 압축행정 말기에 보울 형상에 따라 발생하는 스쿼시 유동이 유동장 변화에 미치는 영향을 조사하고 기존의 실험치 및 수치해석 결과들과 정성적으로 비교하고자 한다.