• Title/Summary/Keyword: 유동 및 구조해석

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An Analysis of Pore Network of Drilling Core from Pohang Basin for Geological Storage of CO2 (이산화탄소 지중저장을 위한 포항분지 시추코어의 공극구조 분석)

  • Park, Jihwan;Park, Hyeong-Dong
    • Tunnel and Underground Space
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    • v.26 no.3
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    • pp.181-191
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    • 2016
  • In geological storage of $CO_2$, the behavior of $CO_2$ is influenced by pore network of rock. In this study, the drilling cores from Pohang Basin were analyzed quantitatively using three-dimensional images acquired by X-ray micro computed tomography. The porosities of sandstone specimens around 740 m-depth (T1), 780 m-depth (T2) and 810 m-depth (T3) which were target strata were 25.22%, 23.97%, 6.28%, respectively. Equivalent diameter, volume, area, local thickness of pores inside the sandstone specimens were analyzed. As a result, the microstructural properties of T1 and T2 specimens were more suitable for geological storage of $CO_2$ than those of T3 specimens. The result of the study can be used as input data of the site for decision of injection condition, flow simulation and so on.

The Formation of Detonation Wave and Acceleration Characteristics with the Ram Accelerator Projectile Shapes (램 가속기 탄체 형상에 따른 데토네이션파와 가속 특성에 관한 연구)

  • 전용희;이재우
    • Journal of the Korean Society of Propulsion Engineers
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    • v.3 no.2
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    • pp.82-91
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    • 1999
  • Projectile shapes of the superdetonative ram accelerator have great effects on shock structures, detonation wave formation, and ram acceleration characteristics. In this study, cone-cylinder-cone, a baseline projectile configuration of the superdetonative combustion mode, double-cone configurations and power-law shape, have been numerically investigated to analyze the effect of the front/rear configuration changes, on the flow field around the projectile, detonation wave formation process, and projectile acceleration characteristics. Hence, a ram projectile configuration with conspicuously improved acceleration characteristics has been proposed by adjusting the double cone angle and height. The results provide useful information for the ram accelerator design optimization study.

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A Study on Performance Improvement of Gear Type Vane Damper in FD Fan - Productivity Increases & Construction Improvement - (FD FAN에서 기어식 베인 댐퍼의 성능개선에 관한 연구 - 생산 및 구조 융합형 기술 -)

  • Jang, Sung-Cheol;Han, Sang-Ho;Kim, Jin-Woo
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.19 no.1
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    • pp.134-139
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    • 2010
  • In this study, we developed the gear type vane damper replacing the link type through gear design using Finite Element Analysis(FEA). FEA about the pinion and the vane shaft in the boss of gear type damper for quality improvement was accomplished. We analyzed fluid flow according to angular displacement. Catched the problem of the torque and backlash bring to the pinion as structure improvement of the forced draft fan(FD FAN). Finally, we compared the gear driving result with simulation. It is the objective of the present study to identify a nonlinear flow rate control of gear type vane damper and to suggest a damper shape with a linear flow rate control. This study is related to the development of gear type vane damper change link type in forced draft fan.

Study of Heat Transfer and Safety Evaluation for Heating Coils in the Fuel Tank of a Ship (선박 연료탱크 내 가온기의 열유동 및 안전성 평가에 관한 해석)

  • Moon, Jin-Gwon;Park, Jong-Chun;Kwon, Yoo-Hong;Yoo, Won-Seok;Ahn, Soo-Whan
    • Journal of Ocean Engineering and Technology
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    • v.24 no.5
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    • pp.22-30
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    • 2010
  • The fuel tank of a ship is filled with heavy fuel oil (HFO) that has a very high viscosity. In order to inject the HFO into the engine easily, heating coils are usually installed inside the fuel tank to heat the HFO and lower its viscosity. Currently, several different types of heating coils are used, e.g., fin-type, bare-type, drum-type, and shell-and-tube-type. It is well known that the shell-and-tube-type heating coil has good performance and high efficiency. In this study, experiments were conducted to determine the heat transfer efficiencies of three different shell-and-tube-type heating coils. Heat transfer efficiency was evaluated by using FLUENT 6.3.26 software. Also, structural safety was assessed by using ANSYS.simulation software.

Performance Evaluation of Multi-Degree-of-Freedom Robotic Mixer using Discrete Element Mixing Simulations (이산요소법 교반 시뮬레이션을 이용한 다자유도 로봇 믹서 성능 평가)

  • Son, Kwon Joong
    • Journal of the Korea Convergence Society
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    • v.11 no.10
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    • pp.219-224
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    • 2020
  • Industrial mixers to homogeneously blend particulate materials have been developed and widely used in various industries. However, most industrial mixers have at most two-degree-of-freedom for the operation, which limits the range of operation parameter selection for optimal blending. This paper proposes a multi-degree-of-freedom robotic mixer designed by converging a conventional drum blender and a robotic manipulator and evaluated its performance in a virtual operating environment. Discrete element simulations were conducted for mixing performance evaluation. The numerical results showed that the proposed mixer design exhibits a better mixing performance than conventional ones.

Comparison Study of Viscous Flutter Boundary for the AGARD 445.6 Wing Using Different Turbulent Boundary Layer Models (난류 경계층 모델을 고려한 AGARD 445.6 날개의 플러터 해석 및 실험결과 비교)

  • Kim, Yo-Han;Kim, Dong-Hyun;Kim, Dong-Man;Kim, Soo-Hyun
    • Journal of the Korea Institute of Military Science and Technology
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    • v.12 no.6
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    • pp.704-710
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    • 2009
  • In this study, a comparison study of flutter analysis for the AGARD 445.6 wing with wind turnnel test data has been conducted in the subsonic, transonic and supersonic flow regions. Nonlinear aeroelastic using FSIPRO3D which is a generalized user-friendly fluid-structure analyses have been conducted for a 3D wing configuration considering shockwave and turbulent viscosity effects. The developed fluid-structure coupled analysis system is applied for aeroelastic computations combining computational structure dynamics(CSD), finite element method(FEM) and computations fluid dynamics(CFD) in the time domain. MSC/NASTRAN is used for the vibration analysis of a wing model, and then the result is applied to the FSIPRO3D module. the results for dynamic aeroelastic response using different turbulent models are presented for several Mach numbers. Calculated flutter boundary are compared with the wind-tunnel experimental and the results show very good agreements.

A Fundamental Study on Development of a Wall Structure type Thermal Diode for Energy Saving (에너지 절약을 위한 벽체형 열다이오드 개발에 관한 기초)

  • Pak, E.T.;Chang, Y.G.;Chea, S.S.
    • Solar Energy
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    • v.17 no.3
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    • pp.67-73
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    • 1997
  • In order to development of a new wall structure type thermal diode for energy saving, the numerical studies have been performed for natural convection across an rectangular enclosure with the various lengthes of the heat source and sink plate. The governing equations for the two-dimensional, laminar, natural convection process in an enclosure are discretized by the control volume approach which insures the conservative characteristics to be satisfied in the calculation domain, and solved by a elliptic SIMPLE algorithm. The momentum and energy equations are coupled through the buoyancy term.

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Analysis of Anisotropic Turbulent Heat Transfer in Nuclear Fuel Bundles (핵연료 집합체내의 비등방성 난류 열전달에 관한 해석적 연구)

  • Kim, Sin;Park, Goon-Cherl
    • Nuclear Engineering and Technology
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    • v.20 no.1
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    • pp.35-46
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    • 1988
  • The prediction of clad surface temperatures is important to the design and the safety anlaysis of nuclear reactor. The accurate prediction requires the detailed knowledge of the flow structure and heat transfer, which is complicate due to anisotropic turbulent phenomena. A two-equation model including anisotropic eddy viscosity model is applied to forecast the velocity distribution. And the temperature field is calculated with uniform wall heat flux. The Galerkin's weighted residual finite element method has been used to calculate the turbulent quantities right up to the wall. The numerical results show good agreement with available data and that turbulence anisotropy strongly affects on the mean flow and thus the temperature field. And Nu-P/D correlation is established for sodium coolant in close-packed equilateral triangular bundle in the P/D range of 1.05 to 1.30.

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Numerical Study on Flame Structure and Pollutant Formation for Syngas Turbulent Nonpremixed Swirl Burner (석탄가스 선회난류 연소기의 화염구조 및 공해물질 배출특성 해석)

  • Lee, Jeong-Won;Kang, Sung-Mo;Kim, Yong-Mo
    • 한국신재생에너지학회:학술대회논문집
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    • 2007.11a
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    • pp.449-452
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    • 2007
  • The present study numerically investigate the effects of the Syngas chemical kinetics on the basic flame properties and the structure of the Syngas diffusion flames. In order to realistically represent the turbulence-chemistry interact ion and the spatial inhomogeneity of scalar dissipation rate. the Eulerian Particle Flamelet Model(EPFM) with multiple flamelets has been applied to simulate the combustion processes and NOx formation in the syngas turbulent nonpremixed flames. Due to the ability for interactively describing the transient behaviors of local flame structures with CFD solver, the EPFM model can effectively account for the detailed mechanisms of NOx format ion including thermal NO path, prompt and nitrous NOx format ion, and reburning process by hydrocarbon radical without any ad-hoc procedure. validation cases include the Syngas turbulent nonpremixed jet and swirling flames. Based on numerical results, the detailed discussion has been made for the sensitivity of the Syngas chemical kinetics as well as the precise structure and NOx formation characteristics of the turbulent Syngas nonpremixed flames.

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Comparison of Experimental and Numerical Analysis for Durability Design Criteria in Ceramic Catalyst Substrate (세라믹 촉매 담체의 내구 설계 기준에 대한 실험 및 수치해석의 비교)

  • Beak, Seok-Heum;Cho, Seok-Swoo
    • Journal of the Korean Society for Precision Engineering
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    • v.27 no.9
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    • pp.58-66
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    • 2010
  • This study examines thermal safety on three-way catalyst that dominates 70 % among whole exhaust gas purification device in 2003. Three-way catalyst durability in the Korea requires 5 years/80,000 km in 1988 but require 10 years/120,000 km after 2002. Three-way catalyst durability in the USA requires 7 years/120,000 km but require 10 years/160,000 km after 2004. Three-way catalyst maintains high temperature in interior domain but maintains low temperature on outside surface. Therefore this device shows tensile stress on outside surface. Temperature distribution of three-way catalyst was acquired by thermal flow analysis for predicted thermal flow parameter. Thermal stress analysis for three-way catalysis was performed based on this temperature distribution. Thermal safety of three-way catalyst was estimated by power law dynamic fatigue life estimation and strength reduction methods for thermal stress.