• 제목/요약/키워드: Gas boundary

검색결과 640건 처리시간 0.036초

Sensitivity of Ba2WO5 to NOx gas at Elevated Temperature

  • Kwak, Mi-Sun;Lee, Joo-Hyeon;Hwang, Jeong-Sug;Park, Chong-Ook
    • The Korean Journal of Ceramics
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    • 제5권2호
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    • pp.110-114
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    • 1999
  • NOx sensing properties of $Ba_2WO_5$ were investigated by varying the sintering temperature in an effort to study the effects of the neck-width on gas sensitivity. $Ba_2WO_5$ sintered at $800^{\circ}C$, which exhibits neck-controlled conduction provides highest sensitivity of 47 and 29 at $500^{\circ}C$ to NO and $NO_2$, respectively. The samples sintered beyond $800^{\circ}C$ show sintering temperature-independent gas sensitivity. This may be because the grain boundary control is dominant at lower sintering temperatures and open neck control is dominant at higher sintering temperatures than $800{\circ}C$. The NOx sensing mechanism of $Ba_2WO_5$ was briefly discussed.

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Expansion of Dusty H II Regions and Its Impact on Disruption of Molecular Clouds

  • Kim, Jeong-Gyu;Kim, Woong-Tae;Ostriker, Eve
    • 천문학회보
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    • 제40권1호
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    • pp.58.3-59
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    • 2015
  • Dynamical expansion of H II regions plays a key role in dispersing surrounding gas and therefore in limiting the efficiency of star formation in molecular clouds. We use analytic methods and numerical simulations to explore expansions of spherical dusty H II regions, taking into account the effects of direct radiation pressure, gas pressure, and total gravity of the gas and stars. Simulations show that the structure of the ionized zone closely follows Draine (2011)'s static equilibrium model in which radiation pressure acting on gas and dust grains balances the gas pressure gradient. Strong radiation pressure creates a central cavity and a compressed shell at the ionized boundary. We analytically solve for the temporal evolution of a thin shell, finding a good agreement with the numerical experiments. We estimate the minimum star formation efficiency required for a cloud of given mass and size to be destroyed by an HII region expansion. We find that typical giant molecular clouds in the Milky Way can be destroyed by the gas-pressure driven expansion of an H II region, requiring an efficiency of less than a few percent. On the other hand, more dense cluster-forming clouds in starburst environments can be destroyed by the radiation pressure driven expansion, with an efficiency of more than ~30 percent that increases with the mean surface density, independent of the total (gas+stars) mass. The time scale of the expansion is always smaller than the dynamical time scale of the cloud, suggesting that H II regions are likely to be a dominant feedback process in protoclusters before supernova explosions occurs.

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RF-diode Sputtering법으로 제작한 Co박막의 자기특성과 미세구조 (Magnetic Properties and Microstructure of Co Thin Films by RF-diode Sputtering Method)

  • 한창석;김상욱
    • 한국재료학회지
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    • 제28권3호
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    • pp.159-165
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    • 2018
  • In order to increase the efficiency of the sputtering method widely used in thin film fabrication, a dc sputtering apparatus which supplies both high frequency and magnetic field from the outside was fabricated, and cobalt thin film was fabricated using this apparatus. The apparatus can independently control the applied voltage, the target-substrate distance, and the target current, which are important parameters in the sputtering method, so that a stable glow discharge is obtained even at a low gas pressure of $10^{-3}$ Torr. The fabrication conditions using the sputtering method were mainly performed in $Ar+O_2$ mixed gas containing about 0.6 % oxygen gas under various Ar gas pressures of 1 to 30 mTorr. The microstructure of Co thin films deposited using this apparatus was examined by electron diffraction pattern and X-ray techniques. The magnetic properties were investigated by measuring the magnetization curves. The microstructure and magnetic properties of Co thin films depend on the discharge gas pressure. The thin film fabricated at high gas pressure showed a columnar structure containing a large amount of the third phase in the boundary region and the thin film formed at low gas pressure showed little or no columnar structure. The coercivity in the plane was slightly larger than that in the latter case.

내산화 및 열차폐 코팅처리 가스터빈 블레이드의 균열거동 (Crack Initiation and Propagation at the Gas Turbine Blade with Antioxidation and Thermal Barrier Coating)

  • 강명수;김준성
    • 한국정밀공학회지
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    • 제27권12호
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    • pp.99-106
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    • 2010
  • Gas turbines operation for power generation increased rapidly since 1990 due to the high efficiency in combined cycle, relatively low construction cost and low emission. But the operation and maintenance cost for gas turbine is high because the expensive superalloy hot gas path parts should be repaired and replaced periodically This study analyzed the initiation and propagation of the crack at the gas turbine blades which are coated with MCrAIY as a bond coat and TBC as a top coat. The sample blades had been serviced at the actual gas turbines for power generation. Total 7 sets of blades were analyzed and they have different EOH(equivalent operation hour). Blades were sectioned and the cracking distribution were measured and analyzed utilizing SEM(scanning electron microscope) and optical microscope. The blades which had 52,000 EOH of operation had cracks at the substrate and the maximum depth was 0.2 mm. Most of the cracks initiated at the boundary layer between TBC and bond coat and propagated down to the bond coat. Once bond coat is cracked, the base metal is exposed to the oxidation condition and undergoes notch effect. Under this environment, the crack branched at the inter-diffusion layer and propagated to the substrate. Critical cracks affecting the blade life were analyzed as those on suction side and platform.

Microstructural Wear Mechanism of $Al_2O_3-5$ vol% SiC nanocomposite and $Si_3N_4$Ceramics

  • Riu, Doh-Hyung;Kim, Yoon-Ho;Lee, Soo-Wohn;Koichi Niihara
    • 한국분말재료학회지
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    • 제8권3호
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    • pp.179-185
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    • 2001
  • Through the observation of wear scar of two ceramic materials, microstructural wear mechanisms was investigated. As for the $Al_2O_3$-5 vol% SiC nanocomposite, the grain boundary fracture was suppressed by the presence of SiC nano-particles. The intragranular SiC particles have inhibited the extension of plastic deformation through the whole grain. Part of plastic deformation was accommodated around SiC particles, which made a cavity at the interface between SiC and matrix alumina. On the other hand, gas-pressure sintered silicon nitride showed extensive grain boundary fracture due to the thermal fatigue. The lamination of wear scar was initiated by the dissolution of grain boundary phase. These two extreme cases showed the importance of microstructures in wear behavior.

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다점 피토관을 이용한 기체 유량 측정의 불확도 평가 (Uncertainty Assessment of Gas Flow Measurement Using Multi-Point Pitot Tubes)

  • 양인영;이보화
    • 한국유체기계학회 논문집
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    • 제19권2호
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    • pp.5-10
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    • 2016
  • Gas flow measurement in a closed duct was performed using multi-point Pitot tubes. Measurement uncertainty was assessed for this measurement method. The method was applied for the measurement of air flow into a gas turbine engine in an altitude engine test facility. 46 Pitot tubes, 15 total temperature Kiel probes and 9 static pressure tabs were installed in the engine inlet duct of inner diameter of 264 mm. Five tests were done in an airflow range of 2~10 kg/s. The flow was compressible and the Reynolds numbers were between 450,000 and 2,220,000. The measurement uncertainty was the highest as 6.1% for the lowest flow rate, and lowest as 0.8% for the highest flow rate. This is because the difference between the total and static pressures, which is also related to the flow velocity, becomes almost zero for low flow rate cases. It was found that this measurement method can be used only when the flow velocity is relatively high, e.g., 50 m/s. Static pressure was the most influencing parameter on the flow rate measurement uncertainty. Temperature measurement uncertainty was not very important. Measurement of boundary layer was found to be important for this type of flow rate measurement method. But measurement of flow non-uniformity was not very important provided that the non-uniformity has random behavior in the duct.

탄소 저장량 감시에서 배수구역과 행정구역의 비교 평가 - 금강산에 대한 UN-REDD 대응 차원에서 - (Comparative Evaluation between Administrative and Watershed Boundary in Carbon Sequestration Monitoring - Towards UN-REDD for Mt. Geum-gang of North Korea -)

  • 김준우;엄정섭
    • 환경영향평가
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    • 제22권5호
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    • pp.439-454
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    • 2013
  • UN-REDD (United Nations programme on Reducing Emissions from Deforestation and forest Degradation) is currently being emerged as one of important mechanism to reduce carbon dioxide in relation to the deforestation. Although administrative boundary has already gained world-wide recognition as a typical method of monitoring unit in the process of GHG (Greenhouse Gas) reduction project, this approach did not provide a realistic evidence in the carbon sequestering monitoring in terms of UN-REDD; the meaningful comparison of land use patterns among watershed boundaries, interpretation for distribution trends of carbon density, calculation of opportunity cost, leakage management, etc. This research proposes a comparative evaluation framework in a more objective and quantitative way for carbon sequestering monitoring between administrative and watershed boundary approaches. Mt. Geumgang of North Korea was selected as a survey objective and an exhaustive and realistic comparison of carbon sequestration between the two approaches was conducted, based on change detection using TM satellite images. It was possible for drainage boundary approach to identify more detailed area-wide patterns of carbon distribution than traditional administrative one, such as estimations of state and trends, including historical trends, of land use / land cover and carbon density in the Mt. Geumgang. The distinctive changing trends in terms of carbon sequestration were specifically identified over the watershed boundary from 4.0% to 34.8% while less than 1% difference was observed in the administrative boundaries, which were resulting in almost 21-22%. It is anticipated that this research output could be used as a valuable reference to support more scientific and objective decision-making in introducing watershed boundary as carbon sequestering monitoring unit.

SNG/Air 예혼합 화염들의 하류상호작용에 있어서 화염 소화 거동에 관한 연구 (A Study on Flame Extinction Behavior in Downstream Interaction between SNG/Air Premixed Flames)

  • 심근선;이기만
    • 한국연소학회지
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    • 제21권4호
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    • pp.48-60
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    • 2016
  • Experimental and numerical studies were conducted to investigate flame behaviors near flammable limits for downstream-interacting SNG-air premixed flames in a counter-flow configuration. The SNG fuel consisted of a methane, a propane, and a hydrogen with volumetric ratios of 91, 6, and 3%, respectively. The most appropriate priority for some reliable reaction mechanisms examined was given to the mechanism of UC San diego via comparison of lean extinction limits attained numerically with experimental ones. Flame stability map was presented with a functional dependencies of lower and upper methane concentrations in terms of global strain rate. The results show that, at the global strain rate of $30s^{-1}$, lean extinction boundary is slanted while rich extinction one is relatively less inclined because of the dependency of such extinction boundary shapes on deficient reactant Lewis number governed by methane mainly. Further increase of global strain rate forces both extinction boundaries to be more slanted and to be shrunk, resulting in an island of extinction boundary and subsequently one flame extinction limit. Extinction mechanisms for lean and rich, symmetric and asymmetric extinction boundary were identified and discussed via heat losses and chemical interaction.

마이크로 초음속 제트 경계층이 레이저가공에서 나타나는 충돌유동에 미치는 영향에 관한 연구 (Study of Effects of the Boundary Layer of Micro-Supersonic Jets on the Flow Impingments in Laser Machining)

  • 유동옥;이열
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2007년도 제29회 추계학술대회논문집
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    • pp.285-288
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    • 2007
  • 레이저가공에서 나타나는 가공부위의 용융된 물질을 밀어내는 가스의 역할을 모사하기 위하여, 구멍이 있는 평판 상부에 충돌하는 마이크로 초음속 제트유동의 경계층 효과가 수치해석적으로 연구되었다. 충돌유동과 충격파의 구조 및 구멍통과 질량유량이 관찰되어 경계층 영향이 고려되지 않은 과거 연구와 비교되었다. 노즐내부 유동의 경계층 효과로 인하여 가공부위 상부에서 보다 강한 마하디스크가 생성되고, 아울러 구멍통과 질량유량도 줄어드는 것이 관찰되었다.

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