• 제목/요약/키워드: H-plane

검색결과 1,298건 처리시간 0.024초

졸-겔법에 의한 $GdAlO_3$ 버퍼층의 제조 (DFabrication of $GdAlO_3$ Buffer Layers by Sol-Gel Processing)

  • 방재철
    • 한국산학기술학회논문지
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    • 제7권5호
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    • pp.801-804
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    • 2006
  • [ $YBa_2Cu_3O_{7-{\delta}}(YBCO)$ ]계 초전도 선재용 $GdAlO_3(GAO)$ 버퍼층을 졸-겔(sol-gel) 공정에 의해 제조하였다. 전구체 용액은 Gd 질산염과 Al 질산염을 1:1 화학양론비로 하여 메탄올에 용해하여 준비하였다. 전구체 용액을 $SrTiO_3(STO)$ (100) 단결정 기판위에 스핀 코팅하고, 수분이 포함된 $N_2-5%\; H_2$ 분위기에서 $1000^{\circ}C$에서 2시간 열처리 하였다. 열처리 후 GAO 층의 표면에 대한 주사전자현미경 관찰에 의해 GAO 층이 에피택셜의 특징인 각면 형상을 갖는 것을 알 수 있었다. X-선 회절분석에 의하면 GAO 버퍼층은 c-축으로 우선 배향된 에피택셜 박막으로써 반가폭이 각각 (002)면에서 $0.29^{\circ}(out-of-plane)$, {112}지면에서 $1.10^{\circ}(in-plane)$의 우수한 배향성을 나타내었다.

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The Study of Different Buffer Structure on Ni-W Tape for SmBCO Coated Conductor

  • Kim, T.H.;Kim, H.S.;Oh, S.S.;Ko, R.K.;Ha, D.W.;Song, K.J.;Lee, N.J.;Yang, J.S.;Jung, Y.H.;Youm, D.J.;Park, K.C.
    • 한국초전도ㆍ저온공학회논문지
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    • 제8권4호
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    • pp.8-11
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    • 2006
  • High temperature superconducting coated conductor has various buffer structures on Ni-W alloy. We comparatively studied the growth conditions of a multi buffer layer $(CeO_2/YSZ/CeO_2)$ and a single buffer layer$(CeO_2)$ on textured Ni-W alloy tapes. XRD data showed that the qualities of in-plane and out-of-plane textures of the two type buffer structures were good. Also, we investigated the properties of SmBCO superconducting layer that was deposited on the two type buffer structure. The SmBCO superconducting properties on the single and multi buffer structure showed different critical current values and surface morphologies. FWHM of In-plane and out-of-plane textures were $7.4^{\circ},\;5.0^{\circ}$ in the top CeO2 layer of the multi-buffer layers of $CeO_2/YSZ/CeO_2$, and $7.3^{\circ},\;5.1^{\circ}$ in the $CeO_2$ single buffer layer. $1{\mu}m-thick$ SmBCO superconducting layers were deposited on two type buffer layer. $I_c$ of SmBCO deposited on single and multi buffer were 90 A/cm, 150 A/cm and corresponding $J_c$ were $0.9MA/cm^2,\;1.5MA/cm^2$ at 77K in self-field, respectively.

ESPI 방법들을 이용한 압력용기 내부 결함 측정에 관한 연구 (A study on the Measurement of Internal Defects of Pressure Vessel by using ESPI Methods)

  • 이정식;강영준;백성훈
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2005년도 춘계학술대회 논문집
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    • pp.1803-1807
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    • 2005
  • The pipe which it uses from the nuclear power plant or factory by a long period use and a corrosive action the inside defect occurs on the inside. abstract here. The ESPI method is in order to investigate the laser light in the measurement object it will be able to measure the wide territory whole in once, does not receive an effect in direction of defect not to be, has the strong point it will be able to measure a change of place arrowhead real-time defect. It measured a inside defect of pressure vessel by using Out of plane ESPI and In plane of ESPI. It compared a each method result.

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3차원 대칭단면 유동장에서의 개선된 난류모델 (Improved Turbulence Model on the 3 Dimensional Plane of Symmetry Flow)

  • 손창현
    • 한국전산유체공학회지
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    • 제2권2호
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    • pp.1-8
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    • 1997
  • Two versions of anisotropic k-ε turbulence model are incorporated in the modified k-ε model of Sohn et al. to avoid the need for the experimental normal stress value in the model and applied to convergent and divergent flows with strong and adverse pressure gradients in the plane of symmetry of a body of revolution. The models are the nonlinear k-ε model of Speziale and the anisotropic model of Nisizima & Yoshizawa. All of the models yield satisfactory results for relatively complex flow on a plane-of-symmetry boundary layer. The results of the models are compared with those results of experimental normal stress value.

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Experimental Analysis of Radiative Heat Interchange on Furnace Exit Plane of a Steam Boiler

  • Ahn, Kook-Young;Antonovsky, Vjacheslav-Ivanovich
    • Journal of Mechanical Science and Technology
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    • 제15권2호
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    • pp.239-247
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    • 2001
  • Measured radiative heat fluxes on the furnace exit plane of a heavy duty power boiler of steam output 1650 T/h are discussed. A high-ash pulverized bituminous coal was used. Such measurements are necessary to improve heat fluxes inside a steam boiler furnace was manufactured. An extra small heat radiation sensor was placed in the water cooled head of the probe. The sensor had no direct contact with furnace gases and measured only the radiant energy. There was no exposure to convective heat transfer. With the radiometric probe, one can obtain a spherical indicatrix of radiation intensity as well as hemispherical radiative heat flux incident on any surface passing through a measuring point inside the furnace. Thus, the quantity of radiation energy, passing through the furnace exit plane, to the convective heating surfaces and the quantity of radiation energy going in the opposite direction were measured. A formula for relative radiative heat flux on the furnace exit plane has been proposed.

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벽면근처에 놓인 정방형주의 유체력 제어 (Fluid Force Suppression of a Square Prism near Plane Wall)

  • 김광석;노기덕;강명훈;변용수
    • 한국마린엔지니어링학회:학술대회논문집
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    • 한국마린엔지니어링학회 2006년도 전기학술대회논문집
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    • pp.61-62
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    • 2006
  • The suppression of fluid force acting on a square prism near plane wall was studied by attaching fences on the comers of the prism. The height of the fence was 10% of the square width and the range of Reynolds number considered was $Re=2.0{\times}10^4$. The experimental parameters were the attaching position and numbers of fences, the space ratios $G/B(G/B=0.1{\sim}1.2)$ between prism and plane wall. The average drag coefficients were increased and the average hit coefficients were decreased and increased with the space ratios foulard plane wall. The drag of the prism was reduced average 7.6% with the space ratios by attaching the normal fence at the rear and upper comer and the horizontal normal fence at the rear and lower corner on the prism.

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플룸에 의한 액체로켓 저부면 복사 가열 해석 (Numerical Analysis on Radiative Heating of a Plume Base in Liquid Rocket Engine)

  • 손채훈;김영목
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 1999년도 추계 학술대회논문집
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    • pp.65-70
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    • 1999
  • Radiative heating of a liquid rocket base plane due to plume emission is numerically investigated. Calculation of flow and temperature fields around rocket nozzle precedes and thereby realistic plume shape and temperature distribution inside the plume are obtained. Based on the calculated temperature field, radiative transfer equation is solved by discrete ordinate method. The averaged radiative heat flux reaching the base plane is about $5kW/m^2$ at the flight altitude of 10.9km. This value is small compared with radiative heat flux caused by constant-temperature (1500K) plume emission, but it is not negligibly small. At higher altitude (29.8km), view factor between the babe plane and the exhaust plume is increased due to the increased expansion angle of the plume. Nevertheless, the radiative heating disappears since the base plane is heated to high temperature (above 1000K) due to convective heat transfer.

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A note on buckling and vibration of clamped orthotropic plates under in-plane loads

  • Felix, D.H.;Bambill, D.V.;Rossit, C.A.
    • Structural Engineering and Mechanics
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    • 제39권1호
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    • pp.115-123
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    • 2011
  • The present work deals with obtaining the critical buckling load and the natural frequencies of clamped, orthotropic, rectangular thin plates subjected to different linear distributed in-plane forces. An analytical solution is proposed. Using the Ritz method, the dependence between in-plane forces and natural frequencies are estimated for various plate sizes, and some results are compared with finite element solutions and where possible, comparison is made with previously published results. Beam functions are used as admissible functions in the Ritz method.

In-Plane형 마이크로니들의 미세사출공정해석 ([ μ ]-Injection Molding Process Analysis for In-Plane Microneedle)

  • 강정진;허영무;정태성;이성희
    • 소성∙가공
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    • 제14권6호
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    • pp.491-495
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    • 2005
  • Micro injection molding analysis for microneedle fabrication was performed in the present study. The dimensions of width and thickness for in-plane microneedle are $600{\mu}m$, $500{\mu}m$, respectively. A delivery system based on guidelines for traditional injection molding was designed for four-cavities molding system. To investigate the effects of processing conditions in the mirconeedle fabrication, injection molding analysis using commercial code was performed. It was shown that the total injection time has a significant effect on the fabrication of in-plane microneedles.

일축압축하에서 포천화강암의 역학적 이방성 (Mechanical Anisotropy of Pocheon Granite under Uniaxial Compression)

  • 박덕원
    • 지질공학
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    • 제15권3호
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    • pp.337-348
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    • 2005
  • 포천 지역에 분포하는 쥬라기 화강암을 대상으로 미세균열 분포특성이 화강암의 역학적 성질에 미치는 영향에 대하여 연구하였다. 3종의 방향성 시편을 대상으로 일축압축시험이 실시되었으며, 각 시편은R(riftplane), G(grain plane) 및 H(hardway plane) 축에 각각 직각이다. 다양한 탄성 상수 중, 3 방향에 따른 포아송비의 변화가 검토되었다 파괴 강도 비-포아송비의 관계도에서 포아송비의 범위는 H-시편에서 가장 높은 분포양상을 보이며 G-시편, R-시편의 순으로 감소한다. 분포곡선은 $I\simIII$ 단계에서는 거의 선형이며, IV-3 단계에서는 기울기의 급격한 증가를 보인다. 관계도에서 보는바와 같이 파괴강도비 $0.92\sim0.96$에서 변곡점이 형성된다. IV-3단계는 탄성 영역의 밖에 속한다. 4단계의 파괴단계에서의 거동은 응력-체적변형율 곡선에서 분석되었다 암석의 거동을 지배하는 응력증분-체적변형율 방정식에서 특징적인 재료상수인 a, n, Q, m 및 $\varepsilon_v^{mcf}$가 결정되었다. 이들 상수중에서 미세균열의 폐합영역( I 단계)에서 고유의 미세균열의 공극률$(a, 10^{-3})$ 그리고 압축지수(n)는 각각 $a^R(3.82)>a^G(3.38)>a^H(2.32)$ 그리고 $n^R(3.69)>n^G(2.79)>n^H(1.99)4의 순서로 나타난다. 특히 IV 단계의 미세균열의 임계체적변형율($\varepsilon_v^{mcf}$)은 3번 면에 수직인 H-시편에서 가장높게 나타난다. 이러한 결과에서 포아송비 및 재료상수와 같은 역학적 성질은 2 조의 미세균열과 밀접한 관계를 보이고있다. 강도 이방성과 미세균열의 방향성과의 상관성은 암석의 파괴 연구에 주요하게 적용될 수 있다.