• 제목/요약/키워드: Solid Flux

검색결과 313건 처리시간 0.025초

KITSAT-1 COSMIC RAY EXPERIMENT-INITIAL RESULTS

  • Min, K.W.;Kim, S.H.;Shin, Y.H.;Choi, Y.W.
    • Journal of Astronomy and Space Sciences
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    • 제10권2호
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    • pp.103-112
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    • 1993
  • The KITSAT-1 was successfully launched on August 11, 1992, into a near circular, 1300-km-high orbit with an $66^{\circ}$inclination. The satellite carries a solid state detector module to measure the high energy particle flux originating mostly from the inner radiation belt. We describe here the objectives of the experiment, the detector structure, and the preliminary result.

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Preparation and Optical Properties of $SrGa_2S_4$:Eu Phosphor

  • 도영낙;배재우;김유혁;양홍근
    • Bulletin of the Korean Chemical Society
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    • 제21권3호
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    • pp.295-299
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    • 2000
  • The photoluminescence and cathodoluminescence of $SrGa_2S_4:EU$ phosphor were optimized with the process and chemical variables (activators, fluxes and reaction temperature) used in solid state reaction. Firing the powder with flux at $800^{\circ}C$ for 2hr gave the highest photoluminescence efficiency under near-UV excitation and the highest cathodoluminescence efficiency of 20.1 lm/W at 2 kV and 33.3 lm/W at 10 kV. The suitability of $SrGa_2S_4:EU$ for application as a phosphor in LCDs and FEDs is discussed.

고체추진제 가스발생기 설계를 위한 필터 효과에 대한 고찰 (On the effect of filters for the design of solid propellant gas generators)

  • 홍문근;이수용
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회B
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    • pp.2524-2527
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    • 2007
  • Solid propellant gas generators (SPGG) play a role as a turbopump starter in liquid propellant propulsion systems by supplying pressurized gas to power turbines for engine start. For such a purpose, the propellants should burn with a relative low flame temperature and the combustion gas should not contain corrosive constituents such as chlorine compounds. In accordance with these requirements, stabilized AN-based propellants have been usually used as the most appropriate oxidizer for propellant compositions. However, the burning area of the propellant intends to increase to satisfy the required mass flux because of its low burning rate. Consequently the burning area incensement brings on the SPGG size augmentation. A flow restriction such as filters is applied to decrease the SPGG size by rising up the combustion pressure resulting in increasing the burning rate. The feasibility of the size reduction of SPGG by the employment of filters have been studied. The preliminary results of this study show that the considerable reduction of SPGG size would be achievable just by installing a filter with relatively high pressure loss coefficient.

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역세척수 회수시스템이 포함된 배출수처리공정의 설계 (Design of Residual Treatment Process with Filter Backwash Recycle System)

  • 배병욱;최경환
    • 한국물환경학회지
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    • 제28권1호
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    • pp.109-114
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    • 2012
  • In this study, both sedimentation and thickening experiments were conducted for residuals produced from an advanced water treatment plant for more accurate and practical design of residual treatment train. In order to design a backwashed residual sedimentation basin (SRSB) in the filter backwash water recycle system, two kinds of backwash waters, one from sand filter (SFBW) and the other from GAC adsorption bed (GACBW), were separately collected and their surface loading rate measured. In addition, in order to design a gravity thickener, batch thickening tests were conducted for concentrated residuals taken from sedimentation basin and their limiting solid flux ($SF_{L}$) measured. From the experimental results and consideration of the seasonal characteristics of the residual, surface loading rate of $70m^{3}/m^{2}{\cdot}d$ was proposed as a design parameter for SRSB and solid loading rate of 20 kg $TS/m^{2}{\cdot}d$ was proposed as a design parameter for gravity thickeners. Finally, the material mass-balance was made for the design of each unit process in the residual treatment train.

상용해석 코드(MSC-Marc)를 활용한 노즐 내열부품의 숯/삭마 해석 기법 (Thermal decomposition and ablation analysis of solid rocket nozzle using MSC.Marc)

  • 김연철
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2009년도 춘계학술대회 논문집
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    • pp.311-314
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    • 2009
  • 고체추진기관의 연소 환경에서 복잡한 형상을 갖는 내열 복합재료의 온도 및 밀도분포를 예측할 수 있는 방법을 개발하였다. 복합재료의 내부 열반응은 Arrhenius 모델을 이용하였으며, 표면 삭마반응은 Zvyagin 이론을 사용하였다. 표면 삭마에 의한 경계조건 및 격자 이동은 Rezoning 기법을 사용하였으며 열분해에 의한 흡열반응 효과는 열분해 가스의 조성비에 기준한 유효 비열 값을 이용하여 계산되었다. 형상이 복잡한 부품으로 이루어진 2차원 축대칭 노즐 조립체에 적용된 방법은 향후 3차원 FEM 열구조 해석에 활용을 목표로 발전될 것이다.

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고체추진기관 연소관단열재의 열파괴 예측기법 (Prediction Method for Thermal Destruction of Internal Insulator in Solid Rocket Motor)

  • 배지열;황인식;강윤구
    • 한국추진공학회지
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    • 제27권1호
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    • pp.9-16
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    • 2023
  • 본 연구에서는 고체추진기관 내 연소관단열재의 열분해와 삭마를 고려하여 단열재의 열응답을 예측할 수 있는 일차원 해석기법을 개발하였다. 모델링에는 연소관단열재 내부에서 발생하는 열분해로 인한 물성변화, 숯층의 팽창 및 분해가스 이동을 고려하였다. 또한 연소가스로부터의 복사/대류 열유속을 경계조건으로 적용하였으며 단열재 표면에서 발생하는 화학적 삭마속도를 대수식으로 모델링하였다. 해석기법 검증을 위해 열전대가 설치된 시험모터에 대한 해석을 수행하였다. 해석으로 도출된 온도분포는 시험과 유사한 값을 나타냈으며 시험과 예측 열파괴두께의 오차는 0.1 mm 내외였다.

활성슬러지조내 부직포 여재 관형필터의 고액분리 특성 평가 (Evaluation of Tubular Type Non-woven Fabric Filter for Solid-liquid Separation in Activated Sludge Reactor)

  • 서규태;이택순;박영미
    • 대한환경공학회지
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    • 제30권2호
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    • pp.234-238
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    • 2008
  • 활성슬러지 공정에 막을 침지한 MBR(Membrane Bioreactor)공정에서 고가의 막을 대체하여 부직포 같은 섬유 여과막을 이용한 연구가 수행되었다. 부직포는 저렴한 가격, 저압에서 높은 투과유속의 확보 등 막을 대체할 수 있는 대안으로서 가치가 높다. 그러나 부직포 여과막 모듈은 막에 비하여 비표면적이 현저하게 작기 때문에 이를 증가시키는 노력이 필요하다. 본 연구에서는 활성슬러지 공정에 부직포 여과 관형 막모듈을 침지하여 설치형태와 관직경에 따라 여과압력에 미치는 영향을 실험적으로 검토하였다. 관형 필터의 직경이 같을 때, 반응조내 필터 모듈의 설치형태가 여과압력 변화에 미치는 영향은 없었다. 그러나 필터의 관 직경이 작을수록 여과압력의 상승이 빠르게 나타났고 이는 관내 수리학적 손실에 기인된 것으로 해석되었다. 따라서 관형 부직포 여과막은 관경 10 mm 이상에서 비표면적을 고려하여 설계하고, 반응조내 수직형으로 설치함이 적정한 것으로 나타났다.

선박용 대형 디젤 엔진 열 해석을 위한 CFD-FEM 연계 방법의 적용 (Application of CFD-FEM Coupling Methodology to Thermal Analysis on the Large-size Marine Diesel Engine)

  • 김한상;민경덕
    • 한국자동차공학회논문집
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    • 제16권1호
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    • pp.64-70
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    • 2008
  • Temperatures of engine head and liner depend on many factors such as spray and combustion process, coolant passage flow and engine related structures. To estimate the temperature distribution of engine structure, multi-dimensional computational fluid dynamics (CFD) codes have been mainly adopted. In this case, it is of great importance to obtain the realistic wall temperature distribution of entire engine structure. In the present work, a CFD-FEM coupling methodology was presented to address this demand. This approach was applied to a real large-size marine diesel engine. CFD combustion and coolant flow simulations were coupled to FEM temperature analysis. Wall heat flux and wall temperature data were interfaced between combustion simulation and solid component temperature analysis via translator by a commercial CFD package named FIRE by AVL. Heat transfer coefficient and surface temperature data were exchanged and mapped between coolant flow simulation and FEM temperature analysis. Results indicate that there exists the optimum cell thickness near combustion chamber wall to reasonably predict the wall heat flux during combustion period. The present study also shows that the effect of cell refining on predicting in-cylinder pressure during combustion is negligible. Hence, the basic guidance on obtaining the wall heat flux needed for the reasonable CFD-FEM coupling analysis has been established. It is expected that this coupling methodology is a robust tool for practical engine design and can be applied to further assessment of the temperature distribution of other engine components.

Surface reactive micro/nano particles on inorganic oxygen separation membrane

  • Lee, Kee-Sung;Shin, Tae-Ho;Lee, Shiwoo;Woo, Sang-Kuk;Yang, Jae-Kyo;Choa, Yong-Ho
    • 한국막학회:학술대회논문집
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    • 한국막학회 2004년도 Proceedings of the second conference of aseanian membrane society
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    • pp.94-97
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    • 2004
  • Micro/nano-sized L $a_{0.6}$S $r_{0.4}$Co $O_{3-}$$\delta$/ particles are considered to improve oxygen permeability in highly selective inorganic oxygen separation membrane. A L $a_{0.7}$S $r_{0.3}$G $a_{0.6}$F $e_{0.4}$ $O_{3-}$$\delta$/ membrane with perovskite structure is fabricated by a conventional solid-state reaction. As the oxygen permeation flux of the L $a_{0.7}$S $r_{0.3}$G $a_{0.6}$F $e_{0.4}$ $O_{3-}$$\delta$/ membrane was lower than commercial gas separation membranes, we coated the L $a_{0.6}$S $r_{0.4}$Co $O_{3-}$$\delta$/ particles to enhance the oxygen permeation flux. It has been demonstrated that the effective area of reactive free surface is an important factor in determining the effectiveness of the introduction of coating layer for oxygen permeation. The introduction of micro/nano L $a_{0.6}$S $r_{0.4}$Co $O_{3-}$$\delta$/ particles was very effective for increasing oxygen flux, as the flux was as much as 2 to 6 times higher than that of an uncoated L $a_{0.7}$S $r_{0.3}$G $a_{0.6}$F $e_{0.4}$ $O_{3-}$$\delta$/ membrane.\delta$/ membrane.>/ membrane.brane.

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고상법을 이용한 Y3Al5O12:Ce3+의 제조에서 BaF2가 미치는 영향 (Effect of BaF2 as a Flux in Solid State Synthesis of Y3Al5O12:Ce3+)

  • 원형석;;원창환;원형일
    • 한국재료학회지
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    • 제21권11호
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    • pp.604-610
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    • 2011
  • The effect of $BaF_2$ flux in $Y_3Al_5O_{12}:Ce^{3+}$(YAG:Ce) formation was investigated. Phase transformation of $Y_3Al_5O_{12}$(YAG) was characterized by using XRD, SEM, and TEM-EDS, and it was revealed that the sequential formation of the $Y_4Al_2O_9$(YAM), $YAlO_3$(YAP) and $Y_3Al_5O_{12}$(YAG) in the temperature range of 1000-1500$^{\circ}C$. Single phase of YAG was revealed from 1300$^{\circ}C$. In order to find out the effect of $BaF_2$ flux, three modeling experiments between starting materials (1.5$Al_2O_3$-2.5$Y_2O_3$, $Y_2O_3$-$BaF_2$, and $Al_2O_3$-$BaF_2$) were done. These modeling experiments showed that the nucleation process occurs via the dissolution-precipitation mechanism, whereas the grain growth process is controlled via the liquid-phase diffusion route. YAG:Ce phosphor particles prepared using a proposed technique exhibit a spherical shape, high crystallinity, and an emission intensity. According to the experimental results conducted in this investigation, 5% of $BaF_2$ was the best concentration for physical, chemical and optical properties of $Y_3Al_5O_{12}:Ce^{3+}$(YAG:Ce) that is approximately 10-15% greater than that of commercial phosphor powder.