• 한국전산유체공학회지
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• 제21권4호
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• pp.19-27
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• 2016

The flow analyses through a porous hydraulic fractures is among the most important tasks in recently developed shale reservoirs but is rendered difficult by non-Darcy effects and geometric changes in the hydraulic fractures during production. In this study, several Computational Fluid Dynamics(CFD) models of hydraulic fractures, with a simple shape such as that of parallel plates, filled with proppants were built. Direct Numerical Simulation(DNS) analyses were then carried out to examine the flow loss characteristics of the fractures. The hydraulic diameters for the simulation models were calculated using the DNS results, and then they were compared with the results from Kozeny's definition of hydraulic diameter which is most widely used in the flow analysis field. Also, the characteristic parameters based on both hydraulic diameters were estimated for the investigation of the flow loss variation features. Consequently, it was checked in this study that the hydraulic diameter based on Kozeny's definition is not accordant to the results from the DNS analyses, and the case using the CFD results exhibits f Re robustness like general pipe flows, whereas the other case using Kozeny's definition doesn't. Ultimately, it is expected that discoveries reported in this study would help further porous flow analyses such as hydraulic fracture flows.

• 한국자동차공학회논문집
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• 제21권6호
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• pp.135-146
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• 2013

This paper presents a feedforward control algorithm for the EGR and VGT systems of passenger car diesel engines. The air-to-fuel ratio and boost pressure are selected as control indicators and the positions of EGR valve and VGT vane are used as control inputs of the EGR and VGT controller. In order to compensate the non-linearity and coupled dynamics of the EGR and VGT systems, we have proposed a non-linear model-based feedforward control algorithm which is obtained from static model inversion approach. It is observed that the average modeling errors of the feedforward algorithm is about 2% using stationary engine experiment data of 225 operating conditions. Using a feedback controller including proportional-integral, the modeling error is compensated. Furthermore, it is validated that the proposed feedforward algorithm generates physically acceptable trajectories of the actuator and successfully tracks the desired values through engine experiments.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제37회 추계학술대회논문집
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• pp.540-543
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• 2011

이단 마이크로 플라즈마 추력기 (${\mu}PT$)의 개념 설계를 위하여 실험적 연구가 수행되었다. 운전 조건 및 노즐의 설계조건에 따른 전극 간격 및 출구 면적의 변화에 대한 추력기의 성능 최적화 연구가 수행되었다. 운전 압력은 $10^{-1}$ Torr에서 $10^{-4}$ Torr의 진공 조건이며 아르곤 가스의 유량은 5 sccm에서 300 sccm에 대하여 추력기의 성능 검증 연구가 이루어 졌다. 소모전력 약 1 watt에서 5 watt의 운전 상태에서 약 3000에서 4000정도의 비추력이 예상된다. 마이크로 플라즈마 추력기에 의해 발생된 토출 제트의 사진 및 전기적 특성에 대한 결과를 포함하였다.

• 한국항공우주학회지
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• 제42권1호
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• pp.29-36
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• 2014

하이브리드 로켓 연소에서는 다양한 종류의 저주파수 연소 압력진동이 나타난다. 10Hz 대역의 저주파수 압력진동은 고체연료와 연소가스의 열 관성 차이 때문에 발생하지만 그외의 저주파수 진동은 고체로켓에서 관찰되는 헬름홀츠 및 $L^*$ 모드에 의해 발생하는 것으로 연소실 부피 변화와 밀접한 관련이 있다. 따라서 유동 특성이 고체로켓과 유사한 하이브리드 로켓 연소에서 연소실 부피 변화는 저주파수 특성에 영향을 미치는 중요한 인자이다. 본 연구에서는 연소실과 후연소실의 형상 변화에 따른 연소 압력의 저주파수 특성 변화를 관찰하였다. 특히 주 연소실과 후연소실의 부피 비가 특정한 값이 되면 연소 도중에 10~30Hz 연소 압력 진동의 진폭이 갑자기 증폭되는 연소불안정 현상이 나타났다. 산화제 유량 조절 및 연료 변경에 의한 O/F 비 변화는 연소 압력의 저주파수 증폭과 무관한 것으로 밝혀졌다. 후연소실로 연소가스가 팽창할 때 발생하는 와류 흘림 현상이 저주파수 불안정 현상과 직접적인 관련 있는 것으로 판단되며 이에 관한 연구가 더 필요하다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2006년도 제27회 추계학술대회논문집
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• pp.139-145
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• 2006

액체추진제로켓엔진(LRE)은 로켓의 궤도 및 동특성 제어에 있어서 가장 중용한 부분 중 하나이다. LRE 제어 목적은 주어진 추력 궤도에 맞추어 추력을 조절하는 것과 주연소실과 가스발생기 내의 연소가스의 온도가 일정 범위를 넘어가지 않도록 추진제의 혼합비를 일정하게 유지시키는 것이다. 이런 제어 목적을 가진 LRE는 LRE를 구성하고 있는 구성품 간의 상호간섭에 의하여 다중제어가 쉽게 이루어지지 않는다. 본 연구에서는 LRE에 대한 동특성 모델을 구성하였으며 PID 제어와 PID+Q-ILC 제어로직을 적용한 결과에 대해 해석하였다. 전산모사 결과, PID 제어 보다 PID+Q-ILC 제어 방식을 적용할 경우 오차를 더욱 더 줄일 수 있는 것을 확인하였다.

• 설비공학논문집
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• 제28권1호
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• pp.21-28
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• 2016

A typical heat exchanger, found in many industrial sites, is made up of a large number of unitary cells, which causes difficulties when carrying out full-scale three-dimensional numerical simulations of the heat exchanger to analyze the aero-thermal performance. In the present study, a three-dimensional numerical study using a porous media model was carried out to evaluate the performance of the heat exchanger modelled in two different ways : full-scale and simplified. The pressure drop in the air side and gas side along with the overall heat transfer rate were calculated using a porous media model and the results were then compared to results obtained with a one-dimensional flow network model. The comparison between the results for two different geometries obtained using a porous media model and a one-dimensional flow network model shows good agreement between the simplified geometry and the one-dimensional flow network model. The full-scale geometry shows reasonable differences caused by the geometry such as sudden expansion and contraction.

• 한국유체기계학회 논문집
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• 제17권3호
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• pp.46-51
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• 2014

In this study, a numerical analysis methodology is studied to predict thermal and flow characteristics of C3X vane with internal cooling. Effects of turbulence models, transition models and viscous work term on temperature and pressure distributions on the vane surface are investigated. These optional terms have few effects on the pressure distributions over the vane surface. However, they have great influence on prediction of the temperature distributions on the vane surface. The combination of k-${\omega}$ based SST turbulence model, ${\gamma}$ transition model and viscous work term are better than RSM turbulence model on prediction of the surface temperature. The average temperature difference between CFD results and experimental results is calculated 2 % at the pressure side and 1 % at the suction side. Furthermore computing time of this combination is half of the RSM turbulence model. When k-${\omega}$ based SST turbulence model and ${\gamma}$ transition model with viscous work term are applied, more accurate predictions of thermal and internal flow characteristics of high pressure turbine are expected.

• 한국결정성장학회지
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• 제13권6호
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• pp.304-308
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• 2003

분리기 내 압력 조절을 통하여 압력 변화가 세라믹 입자 $Al_2O_3$, $Fe_2O_3$ 분급에 미치는 영향을 수치 해석적으로 분석하였다. 입자 분급 해석을 위해 3차원 Lagrangian approach를 이용하였으며, 이를 통해 입자의 분리기 내 거동 경로를 추적하여 각 압력에 따른 분리 가능한 최소 입자 크기(cut-diameter)와 분리율(separation rate)를 계산하였다. 압력 감소는 입자를 운반하는 아르곤 가스의 밀도를 감소시키면서, 분리기 내부 압력 손실을 줄이는 원인이 되었다. 이로 인해 상압에서 분리기 압력이 저압 상태로 변함에 따라, 더 미세한(수 $\mu\textrm{m}$) 입자가 분리 가능함이 예측되었다. 특히 50 torr의 저압 하에서 계산된 세라믹 입자의 분급 양상을 분석하면,$Al_2O_3$ 입자는 4 $\mu\textrm{m}$, $Fe_2O_3$경우는 3$\mu\textrm{m}$ 크기의 입자 분리가 가능하였다.

• Journal of Advanced Marine Engineering and Technology
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• 제38권2호
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• pp.123-132
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• 2014

The maritime sector is advancing with dedicated endeavor to reduce greenhouse gas in addressing issues with regards to global warming. Since 01 January 2013, the International Maritime Organization (IMO) regulation mandatory requirement for Energy Efficiency Design Index (EEDI) has been in place and should be satisfied by newly-built ships of more than 400 gross tonnage and the Ship Energy Efficiency Management Plan (SEEMP) for all ships type. Therefore, compliance to this necessitates planning during the design stage whereas verification can be carried-out through an acceptable method during sea trial. The MEPC-approved 2013 guidance, ISO 15016 and ISO 19019 on EEDI serves the purpose for calculation and verification of attained EEDI value. Individual ships EEDI value should be lower than the required value set by these regulations. The key factors for EEDI verification are power and speed assessment and their synchronization. The shaft power can be measured by telemeter system using strain gage during sea trial. However, calibration of shaft power onboard condition is complicated. Hence, it relies only on proficient technology that operates within the permitted ISO allowance. On the other hand, the ship speed can be measured and calibrated by differential ground positioning system (DGPS). An actual test on a newly-built vessel was carried out to assess the correlation of power and speed. The Energy-efficiency Design Index or Operational Indicator Monitoring System (EDiMS) software developed by the Dynamics Laboratory-Mokpo Maritime University (DL-MMU) and Green Marine Equipment RIS Center (GMERC) of Mokpo Maritime University was utilized for this investigation. In addition, the software can continuously monitor air emission and is a useful tool for inventory and ship energy management plan. This paper introduces the synchronization and identification method between shaft power and ship speed for EEDI verification in accordance with the ISO guidance.

• 한국기계가공학회지
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• 제15권6호
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• pp.129-135
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• 2016

There have been many types of development and commercialization efforts for superconducting power applications with the continuous development of High Temperature Superconducting (HTS) conductors. In particular, HTS power cables are going to be commercialized in real power grids. A cryogenic refrigeration system should be used to keep it below 77 K, and its required cooling capacity continuously increases as the unit length of the HTS power cable increases. Among the many kinds of cryogenic refrigerator, a reverse Brayton refrigerator that uses turbo expanders is a promising refrigerator due to its efficiency and reliability. Among the various components in refrigerators, the cryogenic turbo-expander is the most important part for increasing efficiency and assuring reliability. The design of a 300 W class turbo-expander is described in this paper prior to the development of a 10 kW class turbo expander, which is the required capability for the commercialization of a HTS power cable. The impeller shape and rotation speed are determined based on the cycle analysis. The Eigen frequency and harmonic analysis are conducted with gas bearings at cryogenic temperatures to determine the operational stability.