• 한국지반공학회논문집
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• 제23권12호
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• pp.33-42
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• 2007

연약지반의 강성평가는 샘플링(sampling)과 현장 접근에 따른 교란으로 인해 정확하게 평가하는 것이 상당히 어렵다. 이를 위해 개발된 링 타입 FVP를 이용하여 부산 신항에서 실험이 수행 되었다. 이 논문의 목적은 지반 관입시 발생하는 교란을 최소화 할 수 있도록 기존의 링 타입 FVP를 블레이드 타입 FVP로 개량하는 것이다. 블레이드 타입 FVP는 하단의 웨지 모양, 시료 교란, 트랜스듀서, 케이블의 보호, 그리고 케이블과 트랜스듀서간의 전자기적 커플링을 고려하여 설계하였다. 케이블 간 누화현상은 케이블의 접지와 통합을 통해 제거 할 수 있었다. FVP의 전단파 속도는 초기 도달 시간과 이동거리를 이용하여 간단하게 계산될 수 있었다. FVP 블레이드의 관입에 의한 교란 효과 조사 및 FVP를 통해 측정된 전단파 속도의 타당성을 확인하기 위하여 실내 대형 calibration 챔버를 이용하여 비교 시험을 수행하였다. 블레이드 타입 FVP는 30m 깊이까지 측정이 되었으며, 전단파 속도는 매 심도 10cm마다 측정이 되었다. 본 논문에서 제시된 개량된 블레이드 타입의 FVP는 대상 지반의 교란을 최소화 시키며 현장에서 직접 전단파 속도를 측정 할 수 있는 효과적인 장비라고 할 수 있다.

• 한국해양공학회지
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• 제27권3호
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• pp.67-72
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• 2013

In this study, numerical analyses that considered the dynamic interaction effects between the flow and a turbine were carried out to investigate the power output performance of an H-type Darrieus turbine rotor, which is one of the representative lifting-type vertical-axis tidal-current turbines. For this purpose, a commercial CFD code, Star-CCM+, was utilized for an example three-bladed turbine with a rotor diameter of 3.5 m, a solidity of 0.13, and the blade shape of an NACA0020 airfoil, and the optimal tip speed ratio (TSR) and corresponding maximum power coefficient were evaluated through exhaustive simulations with different sets of flow speed and external torque conditions. The optimal TSR and maximum power coefficient were found to be approximately 1.84 and 48%, respectively. The torque and angular velocity pulsations were also investigated, and it was found that the pulsation ratios for the torque and angular velocity were gradually increased and decreased with an increase in TSR, respectively.

• 한국해양공학회지
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• 제23권2호
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• pp.69-73
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• 2009

The objective of this study was to obtain a better understanding of the delayed hydride cracking (DHC) of Zr-2.5Nb alloy. The DHC model has some defects: first, it cannot explain why the DHC velocity (DHCV) becomes constant regardless of an applied stress intensity factor, even though the stress gradient is affected by the applied stress intensity factor at the notch tip. Second, it cannot explain why the DHCV has a strong dependence on the method of approaching the test temperature by a cool-down or a heating-up, even under the same stress gradient, and third, it cannot predict any hydride size effect on the DHC velocity. The DHC tests were conducted on Zr-2.5Nb compact tension specimens with the test temperatures reached by a heating-up method and a cool-down method. Crack velocities were measured in hydrided specimens, which were cooled from solution-treatment temperatures at different rates by being furnace-cooled, water-quenched, and liquid nitrogen-quenched. The resulting hydride size, morphology, and distributions were examined by optical metallography. It was found that fast cooling rates, which produce very finely dispersed hydrides, result in higher crack growth rates. This different DHC behavior of the Zr-2.5Nb tube with the cooling rate after a homogenization treatment is due to the precipitation of the $\gamma$-hydrides only in the water-quenched Zr-2.5Nb tube. This experiment will provide supporting evidence that the terminal solid solubility of a dissolution (TSSD) of $\gamma$-hydrides is higher than that of $\delta$-hydrides.

• Journal of Advanced Marine Engineering and Technology
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• 제37권6호
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• pp.631-637
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• 2013

기어 끝단과 하우징 사이의 간극이 회전방향으로 편심된 인벌류트펌프에서 체적유량과 유량효율을 검토하였다. 해석은 k-e 모델을 이용하여 FLUENT/R-13을 사용하여 기어의 회전속도, 간극의 거리 및 출구압력이 주어져 있을 경우 난류유동을 해석하였다. 동심축과 편심축의 경우 체적유량을 비롯한 유동특성에 대해 독립변수들의 영향은 지속되었으나 회전방향에 대한 압력 분포는 서로 달라 편심의 경우 상류부에서 대부분의 압력이 상승하고 하류부의 압력은 거의 일정한 특성을 보였으며 편심의 영향이 클수록 이러한 현상은 심하게 나타났다. 편심펌프에서 유동특성은 최소 간극에 의존하며 체적유량 혹은 체적효율은 편심되기 전 동심축보다 크나 최소간극과 같은 크기의 동심펌프보다는 작다. 펌프에서 기어축의 편심에 의한 간극 축소는 펌프성능에 긍정적인 영향을 미칠 수 있다.

• 한국지반공학회:학술대회논문집
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• 한국지반공학회 2007년 가을학술발표회
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• pp.266-292
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• 2007

Round Robin Test (RRT) on ground response analyses was conducted for three sites in Korea based on several site investigation data, which include borehole logs with the N values from standard penetration test (SPT) for all three sites and additionally cone tip resistance profiles for two sites. Three input earthquake motions together with the site investigation data were provided for the RRT. A total of 12 teams participating in this RRT presented the results of ground response analyses using equivalent-linear and/or nonlinear method. Each team determined input geotechnical properties by using empirical relationships and literatures based on own judgment, with the exception of the input motions. Herein, the characteristics of input motions were compared in terms of the frequency and period, and the selection of the depth to bedrock, on which the motions is impinged, was discussed considering geologic conditions in Korea. Furthermore, a variety of geotechnical properties such as shear wave velocity profiles and soil nonlinear curves were investigated with the input properties used in this RRT.

• 대한기계학회논문집
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• 제14권5호
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• pp.1264-1271
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• 1990

본 연구에서는 회전 깃(rotor blade)을 폭 방향과 시위방향으로 많은 평면 페 널(panel)들로 나누어 이에 말굽쇠 형 화류(horseshoe vortex)를 분포시키는 양력면 (lifting surface)으로 대치하고 후류는 깃상의 순환(circulation)분포에 의해 그 크 기가 결정되는 와도(vorticity)를 와류격자로 대치하는 와류격자법(Vortex Lattice Method`VLM)을 사용하여 HAWT의 공기역학적 성능 예측을 시도하였다. 그리고 후류의 형상은 근 후류(near wake)와 원후류(far wake)로 나누어 근 후류는 깃의 후연(trail- ing edge)에서의 속도를 갖고 와선(vortex line)이 움직이게 하여 결정하였고 원 후류 는 반무한대 원형화류 실린더(semi-infinite circular vortex cylinder)로 취급하여 결정하였다.

• 한국군사과학기술학회지
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• 제19권5호
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• pp.618-628
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• 2016

The development of new concepts of liners is required in order to effectively neutralize the enemy's attack power concealed in the armored vehicles. A multiple-layer liner is one of possibilities and has a mechanism for explosion after penetrating the target which is known as "Behind Armor Effect." The multiple-layer explosive liner should have sufficient kinetic energy to penetrate the protective structure and explosive material react after target penetration. With this in mind, double-layer liner materials were obtained by cold spray coating methods and these material properties were experimentally characterized and used in this simulation for double-layer liners. In this study, numerical simulations in the three different layer types, i.e., single, A/B, A/B/A in terms of the layer location were verified in terms of finite element mesh sizes and numerical results for the jet tip velocity, kinetic energy, and the corresponding jet deformation characteristics were analysed in detail depending on the structure of layer types.

• International Journal of Naval Architecture and Ocean Engineering
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• 제5권1호
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• pp.81-100
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• 2013

During the final quarter of the last century considerable efforts have been spent to reduce the hull pressure fluctuations caused by unsteady propeller cavitation. This has resulted in further changes in propeller design characteristics including increased skew, tip unloading and introduction of "New Blade Sections" (NBS) designed on the basis of the so-called Eppler code. An experimental study was carried out to investigate flow characteristics of alternative two-dimensional (2-D) blade sections of rectangular planform, one of which was the New Blade Section (NBS) developed in Newcastle University and other was based on the well-known National Advisory Committee for Aeronautics (NACA) section. The experiments comprised the cavitation observations and the measurements of the local velocity distribution around the blade sections by using a 2-D Laser Doppler Anemometry (LDA) system. Analysis of the cavitation tests demonstrated that the two blade sections presented very similar bucket shapes with virtually no width at the bottom but relatively favourable buckets arms at the suction and pressure sides for the NACA section. Similarly, pressure analysis of the sections displayed a slightly larger value for the NBS pressure peak. The comparative overall pressure distributions around the sections suggested that the NBS might be more susceptible to cavitation than the NACA section. This can be closely related to the fundamental shape of the NBS with very fine leading edge. Therefore a further investigation into the modification of the leading edge should be considered to improve the cavitation behaviour of the NBS.

• Tribology and Lubricants
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• 제34권6호
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• pp.217-225
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• 2018

In this study, we spray a Ni-Cr composite powder onto AISI 4340 steel using the high velocity oxygen fuel method. We subsequently subject the Ni-Cr coating (as-sprayed) to ultrasonic nanocrystal surface modification (UNSM) process to improve the tribological performance. This study aims at increasing the wear resistance and durability of the Ni-Cr coating by altering the surface integrity and microstructure via the UNSM process. The UNSM process reduces the surface roughness of the as-sprayed coating by about 64%, which is explained by observing the elimination of high peaks and valleys and filling up micro-pores. Furthermore, a change in the microstructure of the coating due to continuous high-frequency strikes to the surface by a tip can lead to an increase in hardness from about 48 to 60 HRC. Furthermore, we investigate the characterization of the friction and wear behavior of Ni-Cr coating by a ball-on-disc tribometer in the dry conditions. We determine that after the UNSM process, there is a significant reduction in the friction coefficient of the as-sprayed coating from approximately 1.1 to 0.75. This is owing to the increased hardness and smoothed surface roughness. In addition, we investigate the surface morphology and wear track of the coatings before and after the UNSM process using a scanning electron microscope, energy dispersive spectrometer, and three-dimensional laser scanning microscope. We observe that the wear track of the Ni-Cr coating after the UNSM process is lower than that of the as-sprayed one. Thus, we confirm that the UNSM process has a significant influence on the improvement of the tribological performance of the Ni-Cr composite coating.

• 한국추진공학회지
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• 제11권6호
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• pp.9-17
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• 2007

본 연구에서는 램제트 연소실에서의 재순환 유동이 슬롯 막냉각에 미치는 영향에 대하여 실험을 수행하였다. 램제트 연소실 입구의 경사진 확장면 돌출부에 의해 발생된 재순환 유동이 다단 슬롯 중 첫 번째 슬롯에 영향을 미치도록 실험 장치를 구성하여, 슬롯 출구 하류에서의 속도장, 온도장 및 단열 막냉각 효율을 측정하였다. 재순환 유동의 영향에 들어가는 슬롯에서 분사된 냉각유체는 재순환 유동의 높은 전단력과 난류강도로 인해 분사 직후 급격히 주유동과 혼합되어, 재순환 영역에 포함되지 않은 슬롯보다 냉각 성능이 감소함을 결과를 통해 확인하였다.