• Title/Summary/Keyword: circular section

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Spatial Stability of Non-Symmetric Thin-Walled Curved Beams II : Numerical Approach (비대칭 단면을 갖는 박벽 곡선보의 안정성해석 II : 수치적 방법)

  • 민병철;김문영
    • Computational Structural Engineering
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    • v.11 no.4
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    • pp.253-265
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    • 1998
  • 본 논문에서는 연계논문에서 제시한 비대칭 박벽단면을 갖는 곡선보 및 직선보 이론을 토대로, 곡선보 요소 및 직선보 요소를 개발하고 이를 이용한 유한요소 정식화 과정을 제시한다. 유한요소 정식화 과정에서는 요소의 변위장을 도심에 대하여 정의한 후, 요소 변위벡터에 관한 3차의 Hermitian 다항식을 형상함수로 사용하고 가우스 적분을 행함으로써 탄성 강도행렬 및 기하학적 강도행렬을 산정하였다. 얻어진 강도행렬을 이용하여 고유치 문제를 계산함으로써 좌굴하중을 계산하였으며 다양한 해석 예제를 통하여 다른 연구자들의 해석 결과와 비교 검토함으로써 본 연구의 타당성과 우수성을 입증하고자 한다.

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Thermal Energy Extraction from Phase Change Material - by Means of Finned Thermosyphon - (상변화 물질로부터의 열에너지 추출에 관한 연구 - 핀이 부착된 열싸이폰 이용에 관하여 -)

  • Mok, Jai-Kyun;Yoo, Jai-Suk;Kim, Ki-Hyun
    • Solar Energy
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    • v.8 no.1
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    • pp.5-12
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    • 1988
  • One of the effective means to transfer the heat into and from the energy storage medium is thermosyphon. In this study, a two-phase closed thermosyphon with circular fins was used to extract the thermal energy stored in paraffin wax (Sunoco p-116). Heat transfer characteristics along the heat flow path were investigated as well as the overall performance. Some of the important results are as follows: (1) The temperature distribution of the wax in the radial direction was always maintained fairly uniformly; (2) Compared with bare thermosyphon, the heat transfer rate was vastly improved in the early stage of the experiment; and (3) Heat transfer coefficient between the wax and evaporating section of thermosyphon remained nearly constant during the experiment.

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The Near Field Structure of Initially Asymmetic Jets (비대칭분류의 노즐출구영역에서의 난류유동장 해석)

  • Kim, K.H.;Shin, J.K.;Lee, H.Y.
    • Journal of ILASS-Korea
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    • v.4 no.4
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    • pp.38-45
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    • 1999
  • The near field structure of round turbulent jets with initially asymmetric velocity distribution is investigated experimentally. Experiments were carried out using a constant temperature hot-wire anemometry system to measure streamwise velocity in the jets. The measurements were undertaken across the jet at various streamwise stations in a range starting from the jet exit plane and up to a downstream location of twelve diameters. The experimental results include the distribution of mean and instantaneous velocities, vorticity field, turbulence intensity, and the Reynolds shear stress. The asymmetry of the jet exit plane was obtained by using circular cross-section pipes with a bend at the upstream of the exit. Three pipes were used for this study: A straight pipe, 90 and 160 degree-bended pipes. Therefore, at the upstream of the pipe exit, the secondary flow through the bend and the mean streamwise velocity distribution could be controlled by changing the curvature of pipes.

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P-M Interaction Curve of the Circular Concrete Column Strengthened with CFS (CFS 보강 원형 콘크리트 기둥의 P-M 상관도)

  • 이상호;허원석;김준휘
    • Proceedings of the Korea Concrete Institute Conference
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    • 1998.10b
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    • pp.621-626
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    • 1998
  • In this study, the analytic model of concrete column strengthened with CFS(carbon fiber sheets) for obtaining P-M interaction is presented. Firstly, an algorithm to evaluate accurate behavior of CFS is presented using laminate theory. Stress-strain model of CFS is presented based on the results of this algorithm. Secondly, an algorithm to evaluate stress-strain relationship of concrete column confined with CFS is presented. In order to evaluate the reliability of these algorithms, the results of analysis are compared with experimental data. Lastly, section analysis is performed by using constitutive equations of materials. As a result, P-M interaction curve of the column strengthened is obtained and the strengthening effects of CFs are analyzed.

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A NOTE ON EXTREMAL LENGTH AND CONFORMAL IMBEDDINGS

  • Chung, Bo-Hyun
    • Journal of applied mathematics & informatics
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    • v.28 no.5_6
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    • pp.1315-1322
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    • 2010
  • Let D be a plane domain whose boundary consists of n components and $C_1$, $C_2$ two boundary components of D. We consider the family $F_1$ of conformal mappings f satisfying f(D) $\subset$ {1 < |w| < ${\mu}(f)$}, $f(C_1)=\{|w|=1\}$, $f(C_2)=\{|w|={\mu}(f)\}$. There are conformal mappings $g_0$, $g_1({\in}F_1)$ onto a radial and a circular slit annulus respectively. We obtain the following theorem, $$\{{\mu}(f)|f\;{\in}\;F_1\}=\{\mu|\mu(g_1)\;{\leq}\;{\mu}\;{\leq}\;{\mu}(g_0)\}$$. And we consider the family $F_n$ of conformal mappings $\tilde{f}$ from D onto a covering surfaces of the Riemann sphere satisfying some conditions. We obtain the following theorems, {$\mu|1$ < ${\mu}\;{\leq}\;{\mu}(g_1)$} ${\subset}\;\{{\mu}(\tilde{f})|\tilde{f}\;{\in}\;F_2\}\;{\subset}\;\{{\mu}(\tilde{f})|\tilde{f}\;{\in}\;F_n\}$ and ${\mu}(\tilde{f})\;{\leq}\;{\mu}(g_0)^n$.

Numerical Analysis and Experimental Study for Low Reynolds number region around Micro Air Vehicle (초소형 비행체 주위의 저 레이놀즈수 영역에 대한 수치 해석 및 실험적 연구)

  • Kim Y. H.;Kim W. R.;Kim C.;Rho O. H.
    • 한국전산유체공학회:학술대회논문집
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    • 2002.05a
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    • pp.53-58
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    • 2002
  • A three-dimensional incompressible Navier-Stokes solver is developed for the flow analysis around Micro Air Vehicle(MAV) designed by MACDL(Micro Aerodynamic Control and Design Lab), Seoul National Univ., Validations of this solver are presented for two cases, first flow over the circular cylinder with infinite length, second flow over infinite wing with wing section, E387 airfoil. Simultaneously, Wind Tunnel test is performed with Flatform Wire type sir-component balance and model designed by MACDL. The numerical results are also examined through comparison with experimental data.

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Thermo-elastic stability behavior of laminated cross-ply elliptical shells

  • Patel, B.P.;Shukla, K.K.;Nath, Y.
    • Structural Engineering and Mechanics
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    • v.19 no.6
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    • pp.749-755
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    • 2005
  • In this work, thermo-elastic stability behavior of laminated cross-ply elliptical cylindrical shells subjected to uniform temperature rise is studied employing the finite element approach based on higher-order theory that accounts for the transverse shear and transverse normal deformations, and nonlinear in-plane displacement approximations through the thickness with slope discontinuity at the layer interfaces. The combined influence of higher-order shear deformation, shell geometry and non-circularity on the prebuckling thermal stress distribution and critical temperature parameter of laminated elliptical cylindrical shells is examined.

Stress state around cylindrical cavities in transversally isotropic rock mass

  • Lukic, Dragan C.;Prokic, Aleksandar D.;Brcic, Stanko V.
    • Geomechanics and Engineering
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    • v.6 no.3
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    • pp.213-233
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    • 2014
  • The present paper is dealing with the investigation of the stress field around the infinitely long cylindrical cavity, of a circular cross section, contained in the transversally isotropic elastic continuum. Investigation is based upon the determination of the stress function that satisfies the biharmonic equation, for the given boundary conditions and for rotationaly symmetric loading. The solution of the partial differential equation of the problem is given in the form of infinite series of Bessel's functions. Determination of the stress-strain field around cavities is a common requirement for estimation of safety of underground rock excavations.

Structural Safety Analysis According to the Shape of Door Impact Bar (도어 충격봉의 형상에 따른 구조 안전 해석)

  • Han, Moon-Sik;Cho, Jae-Ung
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.21 no.1
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    • pp.21-25
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    • 2012
  • In this study, the safest model can be selected by the simulation result of structural safety analysis according to the shape of impact bar affected at side door of automobile. The open sectional model of semicircle type has the lowest deformation and stress among 4 kinds of models. As the weight of this model has 30% in comparison with other models, it becomes most economical and stable. As the open sectional model of cap type the highest deformation and stress among 4 kinds of models, it becomes weakest. The closed models with circular and rectangular types has the stress far lower than cap type. The maximum deformation is shown at the center part of impact bar but the maximum stress occurs at the joint part between impact bar and frame.

Convective Heat Transfer of a Paraffin Slurry in a Drag Reducing Carrier Fluid (유동저항 감소유체를 운반유체로 한 파라핀 슬러리의 대류 열전달에 관한 연구)

  • 정동주;최은수
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.13 no.12
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    • pp.1275-1281
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    • 2001
  • Aqueous polymer solutions are known to have small pressure reduction. Paraffin slurries are known to have high thermal capacity. Paraffin particles are mixed into an aqueous polymer solution to make a new heat transfer fluid having high thermal capacity but low pressure reduction. The heat transfer characteristics of the new slurry was tested in a circular tube having a constant heat transfer boundary condition. The new slurry was found to have high Nusselt numbers as well as high thermal capacity and low pressure reduction in the laminar flow. The trends of the Nusselt numbers along the heating test section were studied for various heating conditions.

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