• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제35회 추계학술대회논문집
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• pp.432-437
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• 2010

V-gutter 형 화염안정화장치를 장착한 공기흡입식 엔진의 연소기에서 발생하는 저주파 연소 불안정을 저감시키기 위해 화염안정화장치 뒤쪽에 2차 연료를 분사하는 장치를 고안하였다. 해당 장치는 모델 연소장치를 통해 성공적으로 발생된 110~120 Hz, 180dB 크기의 저주파 연소불안정을 84%까지 저감시키는 데에 성공하였다. 연소불안정의 감소는 2차 연료 공급 유량에만 의존하였으며, 특정 값 이상의 연료 공급량에서만 효과가 나타났다. 이와같은 결과는 2차 연료 공급에 의해 화염안정화장치 뒷면의 화염이 주연료 공급량의 섭동과 독립적으로 유지되어 연소 시스템과 연소기의 음향 시스템의 연계를 끊어주기 때문인 것으로 생각된다.

• 한국항공우주학회지
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• 제44권1호
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• pp.23-32
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• 2016

초고속으로 비행하는 물체의 항력을 줄이기 위해 노즈콘으로부터 제트를 분사하는 다양한 연구가 진행되고 있다. 본 연구에서는 항력감소의 기초자료와 핵심 변수를 파악하기 위해서 미국의 항력감소용 분사 제트 연구 동향을 조사하고 요약하였다. 연구에 활용한 노즈콘 모델의 형상은 반구 실린더, 잘린 콘, 재돌입 캡슐이었으며, 각 모델의 시험조건에 대해 정리하였다. 항력감소의 핵심 변수는 분사제트의 마하수, 질량유량, 압력비율이다. 항력감소효과는 주어진 조건에 따라 다양한 결과를 보였지만, 최대 40~50% 정도까지 항력이 감소하였다.

• International Neurourology Journal
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• 제22권4호
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• pp.275-286
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• 2018

Purpose: OnabotulinumtoxinA (BoNT-A) is a promising therapy for treating neurogenic detrusor overactivity (NDO) in individuals with spinal cord injury (SCI). This systematic review and meta-analysis aimed to carry out an in-depth review and to make an objective estimation of the efficacy and safety of BoNT-A on NDO after SCI. Methods: The PubMed, Embase, and Cochrane databases were searched for all relevant articles published from 2001 to 2016 that referred to NDO, SCI, and BoNT-A or botulinum toxin A. All data were recorded in an Excel spreadsheet by 2 individual reviewers. Review Manager version 5.3 was used to carry out the meta-analysis. Results: This analysis included 17 studies involving 1,455 patients. Compared with placebo and baseline, BoNT-A was effective in increasing maximum cystometric capacity, volume at first involuntary detrusor contraction, cystometric bladder capacity (all P<0.00001), compliance (P=0.001), and the number of patients with complete dryness (P=0.0003), and decreasing detrusor pressure, the number of patients with no involuntary detrusor contractions, the maximum flow rate, the incidence of detrusor overactivity (all P<0.00001), and the number of urinary incontinence episodes (P=0.001). There were no statistically significant differences between doses of 200 U and 300 U or between injections into the detrusor and submucosa. There were no life-threatening adverse events. Conclusions: BoNT-A is effective and safe in treating NDO after SCI. There were no statistically significant differences between doses of 200 U and 300 U or between injecting into the detrusor and submucosa. However, more high-quality randomized controlled trials are still needed.

• 한국기계가공학회지
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• 제20권12호
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• pp.129-135
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• 2021

Injection molding is a manufacturing method of melting the polymer resin and injecting it into a mold to molding it into the desired form. Due to the short molding time and outstanding formability, complex products can be shaped with high precision and it is the most widely used polymer molding method. However, there may be areas that are not filled depending on the location of the injection gate where polymer resin is injected. Formability is determined by deformation and surface precision due to the impact of residual stress after molding. Hence, choosing the location of the injection gate is very important and molding analysis of injection molding is essential to reduce the cost of the mold. This study evaluated the injection formability based on the location of the injection gate of the vertical machining center ATC tool port using injection molding analysis and the results were compared and analyzed. Injection molding analysis was conducted on filling, packing, and deformation according to the location of the gate of the ATC tool port. From each injection gate location, filling time, pressure, and maximum deformation were compared. At gate 2, conditions of molding time and the location of the gate were far superior in production and quality. Gate 2 produced the smallest deformation of 0.779mm with the best quality.

• 도시과학
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• 제11권2호
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• pp.25-30
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• 2022

Resin Transfer Molding FRP (RTM FRP) is a fiber reinforced polymeric plastic which is manufactured by applying pressure to fibers, injecting resin into a mold, and then impregnating it. RTM FRP is a new construction material suitable for producing non-continuum structural elements such as sole plate because it has excellent strength and can produce many members in a short time. In this study, experiments were conducted to estimate the capacity of the bolted connection of RTM FRP. First, a tensile test was conducted to confirm the mechanical properties such as the tensile strength of the RTM FRP to be used for the bolted connection experiments. In addition, experiments were conducted on the bolted connection with the thickness of the RTM FRP and the edge distance of the bolt as variables. In the first experiment, F4.8 bolts were used, and shear failure of the bolt occurred before the RTM FRPs were failed. The F4.8 bolt is a general structural bolts used for the sole plate of a bridge bearing, and it was confirmed that the RTM FRP has a higher bold bearing strength than the shear strength of a F4.8 bolt. In the second experiment, G12.9 bolts were used, and shear failure of the bolt and bearing failure of the RTM FRP occurred simultaneously. In addition, as the thickness of the RTM FRP and the edge length of the bolt increased, the strength of the joint increased. When analogized with the bearing fracture equation of steel plate, the bolted connection of RTM FRP showed a bearing strength coefficient of 0.420 to 0.549 compared to the tensile strength, and it is considered that further research is needed.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2003년도 제20회 춘계학술대회 논문집
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• pp.91-93
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• 2003

A comprehensive numerical study is carried out to investigate for the understanding of the flow evolution and flame development in a supersonic combustor with normal injection of ncumally injecting hydrogen in airsupersonic flows. The formulation treats the complete conservation equations of mass, momentum, energy, and species concentration for a multi-component chemically reacting system. For the numerical simulation of supersonic combustion, multi-species Navier-Stokes equations and detailed chemistry of H2-Air is considered. It also accommodates a finite-rate chemical kinetics mechanism of hydrogen-air combustion GRI-Mech. 2.11[1], which consists of nine species and twenty-five reaction steps. Turbulence closure is achieved by means of a k-two-equation model (2). The governing equations are spatially discretized using a finite-volume approach, and temporally integrated by means of a second-order accurate implicit scheme (3-5).The supersonic combustor consists of a flat channel of 10 cm height and a fuel-injection slit of 0.1 cm width located at 10 cm downstream of the inlet. A cavity of 5 cm height and 20 cm width is installed at 15 cm downstream of the injection slit. A total of 936160 grids are used for the main-combustor flow passage, and 159161 grids for the cavity. The grids are clustered in the flow direction near the fuel injector and cavity, as well as in the vertical direction near the bottom wall. The no-slip and adiabatic conditions are assumed throughout the entire wall boundary. As a specific example, the inflow Mach number is assumed to be 3, and the temperature and pressure are 600 K and 0.1 MPa, respectively. Gaseous hydrogen at a temperature of 151.5 K is injected normal to the wall from a choked injector.A series of calculations were carried out by varying the fuel injection pressure from 0.5 to 1.5MPa. This amounts to changing the fuel mass flow rate or the overall equivalence ratio for different operating regimes. Figure 1 shows the instantaneous temperature fields in the supersonic combustor at four different conditions. The dark blue region represents the hot burned gases. At the fuel injection pressure of 0.5 MPa, the flame is stably anchored, but the flow field exhibits a high-amplitude oscillation. At the fuel injection pressure of 1.0 MPa, the Mach reflection occurs ahead of the injector. The interaction between the incoming air and the injection flow becomes much more complex, and the fuel/air mixing is strongly enhanced. The Mach reflection oscillates and results in a strong fluctuation in the combustor wall pressure. At the fuel injection pressure of 1.5MPa, the flow inside the combustor becomes nearly choked and the Mach reflection is displaced forward. The leading shock wave moves slowly toward the inlet, and eventually causes the combustor-upstart due to the thermal choking. The cavity appears to play a secondary role in driving the flow unsteadiness, in spite of its influence on the fuel/air mixing and flame evolution. Further investigation is necessary on this issue. The present study features detailed resolution of the flow and flame dynamics in the combustor, which was not typically available in most of the previous works. In particular, the oscillatory flow characteristics are captured at a scale sufficient to identify the underlying physical mechanisms. Much of the flow unsteadiness is not related to the cavity, but rather to the intrinsic unsteadiness in the flowfield, as also shown experimentally by Ben-Yakar et al. [6], The interactions between the unsteady flow and flame evolution may cause a large excursion of flow oscillation. The work appears to be the first of its kind in the numerical study of combustion oscillations in a supersonic combustor, although a similar phenomenon was previously reported experimentally. A more comprehensive discussion will be given in the final paper presented at the colloquium.

• Journal of Dental Anesthesia and Pain Medicine
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• 제20권4호
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• pp.195-202
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• 2020

Background: Nasotracheal intubation is the most commonly used method to secure the field of view when performing surgery on the oral cavity or neck. Like orotracheal intubation, nasotracheal intubation uses a laryngoscope. Hemodynamic change occurs due to the stimulation of the sympathetic nervous system. Recently, video laryngoscope with a camera attached to the end of the direct laryngoscope blade has been used to minimize this change. In this study, we investigated the optimal effect-site concentration (Ce) of remifentanil for minimizing hemodynamic responses during nasotracheal intubation with a video laryngoscope. Methods: Twenty-one patients, aged between 19 and 60 years old, scheduled for elective surgery were included in this study. Anesthesia was induced by slowly injecting propofol. At the same time, remifentanil infusion was initiated at 3.0 ng/ml via target-controlled infusion (TCI). When remifentanil attained the preset Ce, nasotracheal intubation was performed using a video laryngoscope. The patient's blood pressure and heart rate were checked pre-induction, right before and after intubation, and 1 min after intubation. Hemodynamic stability was defined as an increase in systolic blood pressure and heart rate by 20% before and after nasotracheal intubation. The response of each patient determined the Ce of remifentanil for the next patient at an interval of 0.3 ng/ml. Results: The Ce of remifentanil administered ranged from 2.4 to 3.6 ng/ml for the patients evaluated. The estimated optimal effective effect-site concentrations of remifentanil were 3.22 and 4.25 ng/ml, that were associated with a 50% and 95% probability of maintaining hemodynamic stability, respectively. Conclusion: Nasotracheal intubation using a video laryngoscope can be successfully performed in a hemodynamically stable state by using the optimal remifentanil effect-site concentration (Ce₅₀, 3.22 ng/ml; Ce₉₅, 4.25 ng/ml).

• Korean Chemical Engineering Research
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• 제47권1호
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• pp.133-140
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• 2009

본 연구에서는 투과도 80 md, 하이드레이트 포화도 30%의 다중공 평판형 시스템에서 열자극 감압법에 의한 생산실험을 수행하여 하이드레이트의 해리양상 및 생산효율을 관측 및 분석하였다. 감압의 크기에 따른 실험결과에서, 운영 압력을 낮게 설정하면 높은 가스회수율을 얻을 수 있지만 생산초기 나타나는 강한 펄스가 생산전 운영에 무리를 줄 수 있다고 판단되었다. 또한 흡열반응에 의한 하이드레이트 재형성으로 오히려 회수율이 감소하는 경우가 발생하였다. 감압법 적용시의 생산거동을 더 상세히 분석하기 위해, 감압크기 140 psi와 320 psi에 대해 각각 4, 6회의 반복실험을 진행하였다. 그 결과, 140 psi로 감압크기를 설정한 경우, 생산초기에 불안정한 거동이 나타나지만, 빠르게 안정화됨을 알 수 있었다. 320 psi의 실험결과에서 불연속적이며 간헐적인 생산거동을 확인할 수 있었다. 열자극 실험은 안정적인 생산거동을 보이며 회수율이 비교적 낮아 열자극의 효과를 잘 관찰할 수 있는 압력차 80 psi를 적정운영 압력으로 설정하여 수행하였다. 열자극감압 혼용기법의 결과로부터 열자극시간이 증가할수록 가스회수율은 증가하였지만, 반면 에너지효율은 오히려 감소하는 것으로 나타났다. 열을 2분간 가한 후 열흡수 시간을 1분으로 설정한 경우 본 시스템에서는 회수율이 상승하였으며, 에너지효율 또한 증가되는 결과를 얻었다. 하지만, 열흡수 시간이 1분 이상일 경우 오히려 더 낮은 회수율과 에너지효율을 보였는데 이는 긴 열흡수 시간으로 인한 열손실에 기인한 것으로 판단된다.

• Restorative Dentistry and Endodontics
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• 제36권5호
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• pp.377-384
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• 2011

연구목적: 본 연구의 목적은 열연화주입형 gutta percha와 resilon의 온도 변화에 따른 점탄성 변화를 관찰하고 조작성을 비교하기 위함이다. 연구 재료 및 방법: Obtura-II 시스템을 이용하여 세 종류의 gutta percha와 resilon을 $140^{\circ}C$와 $200^{\circ}C$로 가열한 후 사출 온도를 측정하였다. 점도계를 이용하여 온도 변화에 따른 재료들의 점탄성 특성(전단탄성계수, G'; 전단점성계수, G"; 손실 탄젠트, tan${\delta}$; 복소점도, ${\eta}^*$)을 관찰하였다. 점도계와 차동주사열측정기(DSC)로 재료들의 상전이 온도를 측정하였고 가압법으로 $60^{\circ}C$와 $40^{\circ}C$에서 재료들의 점조도를 비교하였다. 결과: 세 종의 gutta perchas는 온도에 따라 서로 다른 점탄성 특성을 나타냈다. $40-50^{\circ}C$에서 연화된 재료의 고체화 상변이가 일어났고, 점도계와 DSC로 측정된 상변이 시작 온도는 유사하였다. 상변이 시작 온도와 가압 시 점조도는 재료들마다 차이를 보였다(p < 0.05). Resilon은 gutta percha와 비슷한 유변학적 특성을 보였다. 결론: 열연화된 근관충전재는 냉각과정 동안 유변학적 특성의 변화를 나타냈고 재료들마다 서로 다른 점탄성 특성은 근관 내주입 시와 충전 시 서로 다른 조작성을 보임을 알 수 있다.

• 한국항공우주학회지
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• 제44권4호
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• pp.343-351
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• 2016

초임계 환경에서 작동하는 와류형 분사기의 극저온 질소 분무특성을 3차원 LES 수치기법을 적용하여 연구하였다. 초임계 상태에서 질소의 상태량을 예측하기 위해 초임계 상태에서 적용되는 상태방정식들을 비교하여 가장 정확한 SRK 상태방정식을 적용하였다. 또한 점성계수와 열 전도도는 Chung이 제안한 고압상태 혼합물에 대한 방정식을 적용하였으며 확산계수는 Fuller의 이론에 Takahashi가 제안한 방정식을 적용하였다. 질소로 채워진 50bar의 챔버에 5bar의 차압으로 질소를 분무하여 수치해석을 수행하였다. FFT를 이용한 주파수 분석을 통해 대수적 Smagorinsky와 동적 Smagorinsky를 실험결과와 비교하여 동적모델이 더 적합함을 판단하였다. 분사기 내부의 액막, 가스층에서 나타나는 불안정성과 분사기 외부에서 나타나는 불안정성의 원인에 대해 분석하고, 불안정성이 분사기 내부로 전파되는 현상에 대해 조사하였다. 또한 분무각에 대하여 실험 결과와 비교 검증하였다.