• 제목/요약/키워드: plane axisymmetric

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축대칭 쉘구조물의 형상 설계민감도 해석 및 최적설계 (Shape Design Sensitivity Analysis and Optimization of Axisymmetric Shell Structures)

  • 김인용;곽병만
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 1993년도 가을 학술발표회논문집
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    • pp.98-105
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    • 1993
  • A method for shape design sensitivity analysis for axisymmetric shells of general shapes is developed. The basic approach is to divide the structures into many segments. For each of the segments, the formula for a shallow arch or shell can be applied and the results assembled. To interconnect those segments, the existing sensitivity formula, obtained for a variation only in the direction perpendicular to the plane on which the structure is mapped, has been extended to include a variation normal to the middle surface. The method follows the adjoint variable approach based on the material derivative concept as established in the literature. Numerical examples are taken to illustrate the method and the applicability to practical design problems.

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에너지 저장시스템용 복합재 플라이휠 로터의 설계 (Design of a Composite Flywheel Rotor for Energy Storage System)

  • 정희문;최상규;하성규
    • 대한기계학회논문집
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    • 제19권7호
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    • pp.1665-1674
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    • 1995
  • An optimum design has been performed to maximize specific energy (SED) of composite flywheel rotor for energy storage system. The flywheel rotor is assumed to be an axisymmetric thick laminated shell with a plane strain state for structural analysis. For the structural analysis the centrifugal force is considered and the stiffness matrix equation was derived for each ring considering the interferences between the rings. The global stiffness matrix was derived by integrating the local stiffness matrix satisfying the conditions of force and displacement compatibilities. Displacements are then calculated from the global stiffness matrix and the stresses in each ring are also calculated. 3-D intra-laminar quadratic Tsai-Wu criterion is then used for the strength analysis. An optimum procedure is also developed to find the optimal interferences and lay up angle to maximize SED using the sensitivity analysis.

열경화성 고분자 복합재 구조물의 축대칭 유한요소해석 (Axisymmetric Finite Element Analysis of Decomposing Polymeric Composites and Structures)

  • 이선표
    • 연구논문집
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    • 통권24호
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    • pp.81-96
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    • 1994
  • To investigate failure mechanisms observed in carbon-phenolic thermal insulators, differential equations which govern the decomposition process in a deformable anisotropic porous solid are derived for three-dimensional axisymmetric constructions. The governing equations not only couple the material deformation with pore pressure, but also couple pressure and temperature, which means that heat convected by the pyrolysis gases is properly accounted for. Then the Bubnov-Galerkin finite element method is applied to these equations to transform them into a semidescrete finite element system. A thermal insulation liner in the cowl region under typical operating conditions is analyzed to find a mechanism for plylift. The results from the structural analysis show across-ply failure in the cowl zone. The mechanism for plylift is hypothesized as a sequential procedure : 1) the across-ply failure which is the precursor to plylift and 2) the local fiber buckling caused by generation of excessive in-plane compressive stress. To prevent plylift, the across-ply stress can be reduced by using appropriate material ply angles in cowl zone design.

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발달 단계의 축대칭 열대저기압의 각운동량에 관한 연구 (Study on the Angular Momentum of Axisymmetric Tropical Cyclone in the Developing Stage)

  • 강현규;정형빈
    • 대기
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    • 제23권1호
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    • pp.1-11
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    • 2013
  • The angular momentum transport of an idealized axisymmetric vortex in the developing stage was investigated using the Weather Research and Forecast (WRF) model. The balanced axisymmetric vortex was constructed based on an empirical function for tangential wind, and the temperature, geopotential, and surface pressure were obtained from the balanced equation. The numerical simulation was carried out for 6 days on the f-plane with the Sea Surface Temperature (SST) set as constant. The weak vortex at initial time was intensified with time, and reached the strength of tropical cyclone in a couple of days. The Absolute Angular Momentum (AAM) was transported along with the secondary circulation of the vortex. Total AAM integrated over a cylinder of radius of 2000 km decreased with simulation time, but total kinetic energy increased rapidly. From the budget analysis, it was found that the surface friction is mainly responsible for the decrease of total AAM. Also, contribution of the surface friction to the AAM loss was about 90% while that of horizontal advection was as small as 8%. The trajectory of neutral numerical tracers following the secondary circulation was presented for the Lagrangian viewpoint of the transports of absolute angular momentum. From the analysis using the trajectory of tracers it was found that the air parcel was under the influence of the surface friction continuously until it leaves the boundary layer near the core. Then the air parcel with reduced amount of angular momentum compared to its original amount was transported from boundary layer to upper level of the vortex and contributed to form the anti-cyclone. These results suggest that the tropical cyclone loses angular momentum as it develops, which is due to the dissipation of angular momentum by the surface friction.

스파이크 노즐 설계 (SHAPING A NOZZLE WITH A CENTRAL BODY)

  • 김철웅
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2005년도 추계 학술대회논문집
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    • pp.293-298
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    • 2005
  • We calculate the coordinates of an axisymmetric nozzle with a central body. This nozzle ensures a transonic flow with a plane sound surface, which is orthogonal to the symmetry axis and has a wall kink at the sonic point, The Chaplygin transformation in the subsonic part of the flow leads the Dirichlet problem for a system of nonlinear equations. The definition domain of the solution in the velocity-hodograph plane is taken as a rectangle. This enables one to obtain the nozzle with a monotonic distribution of velocity along its subsonic part. In the nonlinear differential equation, the linear Chaplygin operator for plane flows is separated, which allows the iterative calculation of the solution. The supersonic part of the nozzle is calculated under the assumption that the flow at the nozzle exit is uniform and parallel to the symmetry axis; i.e., the supersonic jet outflows to the submerged space with the same pressure. The calculation is performed by the characteristic method. The exact solution of Tricomi equation for near-sonic flows with the straight sonic line is used to 'move away' the sound plane. The velocity distribution alone the supersonic part of the nozzle is also monotonic, which ensures the absence of the boundary-layer separation and, therefore, the adequacy of the ideal-gas model. calculations show that the flow in the supersonic part of the nozzle is continuous (compression shocks are absent)

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탄소성 동적해석시 해에 미치는 여러 인자들의 비교연구 (A Comparative Study on Elastic-Plastic -Dynamci Analysis of Sheet Metal Forming)

  • 박종진
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 1999년도 춘계학술대회논문집
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    • pp.245-248
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    • 1999
  • Explicit dynamic finite element analysis has been used widely in the field of sheet metal forming. However in using the analysis technique there are some parameters which are not clearly defined so that engineers may obtain inaccurate solutions In the present study parameters such as time step damping ratio penalty constant and punch speed were investigated on their influence to the solution behavior. Considered forming processes are plane stain bending by a punch and axisymmetric deep drawing.

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유한요소법을 이용한 초소성 성형공정 해석 (Analysis of Superplastic Forming Processes U sing Finite Element Method)

  • 홍성석;김민호;김용환
    • 대한기계학회논문집
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    • 제19권6호
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    • pp.1411-1421
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    • 1995
  • A rigid visco-plastic finite element method has been developed for modeling superplastic forming processes. The optimum pressure-time relationship for a target strain rate and thickness distributions was predicted using two-node line element based on membrane approximation for plane strain and axisymmetric condition. Analysis of superplastic forming was carried out using the developed program and the numerical results were compared to the values available in the literature for plane strain problems. For description of the contact between the dies and sheet, the direct projection method was applied to the complicated problem and the validity of the scheme was tested. Experiments for the various geometries such as hemisphere and cone were performed with the developed forming machine using the calculated optimum pressure-time curves. Comparison between analysis and experiments showed good agreement.

A Closed-Form Solution for Circular Openings in an Elastic-Brittle-Plastic Extended Spatial Mobilized Plane Medium

  • Wu, Chuangzhou;Guo, Wei;Jang, Bo-An
    • 지질공학
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    • 제32권1호
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    • pp.1-12
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    • 2022
  • Based on the extended spatial mobilization plane (SMP) criterion, we present an elastic-brittle-plastic solution for an axisymmetric cylindrical tunnel. The influences of the intermediate principal compressive stress and material strain-softening behavior are considered. Closed-form formulas for the critical support force, radius of plastic zone, and distributions of stress and displacement in surrounding rock are proposed. The elastic-plastic solution based on SMP is compared with the Kastner solution to verify the credibility of the obtained elastic-plastic solution. The elastic-brittle-plastic solution following the SMP criterion and the current solution based on the Mohr-Coulomb criterion are also compared. The rock strain-softening rate and the intermediate principal stress affect the stability of the surrounding rock. The results provide guidance for optimizing the design of support systems for tunnels.

MW급 풍력발전기 동력전달용 테이퍼 연결장치 설계에 관한 연구 (Tapered Joint Design for Power Transmission of MW-grade Wind Turbine)

  • 강종훈;배준우;온한용;권용철
    • 대한기계학회논문집A
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    • 제39권11호
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    • pp.1183-1189
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    • 2015
  • 본 연구는 풍력발전기용 동력 전달부품의 테이퍼 연결장치 설계에 관한 것이다. 요구되는 전달토크의 크기, 동력을 전달하는 축의 직경, 테이퍼 링의 접촉면적 그리고 압축 면압을 부과하기 위한 볼트의 체결력 등이 테이퍼 연결장치 설계의 주요 변수이다. 테이퍼 연결의 계산은 축대칭 평면 변형률 조건의 복합링 구조로 가정하여 응력과 변형량을 계산 하였다. 축에 작용하는 면압은 요구 전달동력을 이용하여 계산하였고, 보강링에 작용하는 면압은 축과 허브의 변형량 일치 조건을 이용하여 계산하는 방법을 제안하였다. 복합링의 수식으로 구한 반경방향의 변형량으로 테이퍼 각도를 고려한 축방향 습동거리를 계산하였다. 수식으로 구한 응력과 상대습동거리의 타당성을 검증하기 위하여 유한요소해석을 수행하였으며 축방향의 하중이 발생하는 테이퍼면에서 원주방향의 응력이 최대 10% 수준의 오차를 보이고 있으나 그 외 응력분포와 상대습동거리는 수식적인 방법과 해석적인 방법이 일치함을 확인하였다.

교량구간에서의 경량전철에 의한 지반진동 해석 (Ground Vibration Analysis for Light Rail Transit on Bridges)

  • 김두기;이종재;윤정방;김두훈
    • 한국지반공학회논문집
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    • 제16권4호
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    • pp.71-82
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    • 2000
  • 본 연구에서는 교량구간에서 경량전철의 주행에 의한 지반진동해석방법을 제안하였다. 경량전철의 주행시 교각에 작용하는 동하중을 열차와 교량의 상호작용을 고려하여 구하였으며, 경량전철 동하중에 의한 인근의 지반진동을 평면내 파동 전파와 축대칭 파동전파 해법을 사용하여 구한 후 비교/분석하였다. 또한, 축대칭 진동해석결과를 선형조합한 보다 엄밀한 교량구간에서의 지반진동해석법을 제시하였으며, 이를 통해 인접교각이 지반진동에 미치는 영향을 고찰하였다. 아울러 경량전철의 운행에 따른 환경진동의 문제를 평가하기 위하여 상판재료와 지반조건 등 제반사항의 변화에 따른 지반진동의 변화를 살펴보았다.

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