• 제목/요약/키워드: higher order solution

검색결과 1,044건 처리시간 0.026초

고차 등매개요소에서 내부절점의 위치와 해의 안정성 연구 (A study on the solution stability by the position of internal nodes in hihger order isoparametric elements)

  • 이준희;임장근
    • 대한기계학회논문집A
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    • 제21권12호
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    • pp.1973-1983
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    • 1997
  • Higher order isoparametric elements are usually used in the finite element analysis because they can represent easily the geometric shape of a complex structure ad can improve the solution quality. When these elements are used, the position of internal nodes affects greatly on the solution accuracy. Decreasing of the accuracy related to the position of internal nodes is due to non-conformal mapping often results in an unstable Jacobian value. This paper, in order to remove this difficulty, suggests a modified shape function which can establish conformal mapping between two coordinate systems. Numerical experiments with the proposed shape function show that a stable solution can be obtained without respect to the position of internal nodes, and offer convenience that one can take arbitrarily the position of internal nodes considering only the geometric shape of element boundaries.

Analytical solution for buckling of embedded laminated plates based on higher order shear deformation plate theory

  • Baseri, Vahid;Jafari, Gholamreza Soleimani;Kolahchi, Reza
    • Steel and Composite Structures
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    • 제21권4호
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    • pp.883-919
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    • 2016
  • In this research, buckling analysis of an embedded laminated composite plate is investigated. The elastic medium is simulated with spring constant of Winkler medium and shear layer. With considering higher order shear deformation theory (Reddy), the total potential energy of structure is calculated. Using Principle of Virtual Work, the constitutive equations are obtained. The analytical solution is performed in order to obtain the buckling loads. A detailed parametric study is conducted to elucidate the influences of the layer numbers, orientation angle of layers, geometrical parameters, elastic medium and type of load on the buckling load of the system. Results depict that the highest buckling load is related to the structure with angle-ply orientation type and with increasing the angle up to 45 degrees, the buckling load increases.

nconel 600위에 증착된 TiN 박막의 고온 NaCl 수용액에서의 CPP 실험에 의한 핏팅저항성의 연구 (A Study on Pitting Resistance of TiN Film Coated on Inconel 600 by CPP Test in High Temperature NaCl Solution)

  • 김용일;정한섭;김홍회;이원종
    • 한국세라믹학회지
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    • 제32권11호
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    • pp.1301-1307
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    • 1995
  • Pitting corrosion of TiN film deposited on Inconel 600 by plasma assisted chemical vapor deposition (PACVD) was investigated. Cyclic potentiodynamic polarization (CPP) tests were conducted in order to determine the pit nucleation potentials, Enp, of the TiN-deposited sample and the bare Inconel 600 in deaerated NaCl solution at 25, 135 and 20$0^{\circ}C$. The effects of the TiN film thickness, the solution temperature and the Cl- concentration on Enp were studied. Enp of the TiN-deposited sample which had the film thickness above 1${\mu}{\textrm}{m}$ were higher than those of the bare Inconel 600 by 300~600mV at all the solution temperatures, implying the pitting resistance improvement of the TiN film. The morphologies of the pits generated after immersion test were examined with a scaning electron microscopy. The higher was the solution temperature, the more corrosion products, mainly composed of Cr and Ni oxides, were formed.

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A Study on the Generation of Capillary Waves on Steep Gravity Waves

  • Lee, Seung-Joon
    • Journal of Ship and Ocean Technology
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    • 제4권4호
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    • pp.45-55
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    • 2000
  • A formal solution method using the complex analysis is given for the problems derived by Longuet-Higgins(1963). The same method is applied to a new perturbation problem of higher approximation. Interpretation of its solution made it possible to confirm that the rough agree-ment of Longuet-Higgins\`s prediction with experimental data of Cox(1958) was mainly due to the fact that the gravity effect in the perturbation problem was neglected for the case when the basic gravity wave not sufficiently steep.

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비선형제어계의 선형화에 의한 근사해의 연구 (Approximation method of nonlinear control system by linearization)

  • 양흥석;김경기
    • 전기의세계
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    • 제22권1호
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    • pp.28-34
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    • 1973
  • This paper treats with the sub-optimal control problem of noninear systems by approximation method. This method involves the approximation by linearization which provides the sub-optimal solution of non-linear control problems. The result of this work shows that, in the problem in which the controlled plant is characterized by an ordinary differential equation of first order, the solution obtained by this method coincides with the exact solution of problem. In of case of the second or higher order systems, it is proved analytically that this method of linearization produces the sub-optimal solution of the given problem. It is also shown that the sub-optimality of solution by the method can be evaluated by introducing the upper and lower bounded performance indices. Discussion is made on the procedure with some illustrative examples whose performance indices are given in the quadratic forms.

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OSCILLATION OF HIGHER ORDER STRONGLY SUPERLINEAR AND STRONGLY SUBLINEAR DIFFERENCE EQUATIONS

  • Grace, Said R.;Han, Zhenlai;Li, Xinhui
    • Journal of applied mathematics & informatics
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    • 제32권3_4호
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    • pp.455-464
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    • 2014
  • We establish some new criteria for the oscillation of mth order nonlinear difference equations. We study the case of strongly superlinear and the case of strongly sublinear equations subject to various conditions. We also present a sufficient condition for every solution to be asymptotic at ${\infty}$ to a factorial expression $(t)^{(m-1)}$.

프로펠러 단독성능해석 향상을 위한 고차패널법의 적용 (Application of High Order Panel Method for Improvement of Prediction of Marine Propeller Performance)

  • 김건도;이창섭
    • 대한조선학회논문집
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    • 제42권2호
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    • pp.113-123
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    • 2005
  • A higher order panel method based on B-spline representation for both the geometry and the solution is developed for the analysis of steady flow around marine propellers. The self-influence functions due to the normal dipole and the source are desingularized through the quadratic transformation, and then shown to be evaluated using conventional numerical quadrature. By selecting a proper order for numerical quadrature, the accuracy of the present method can be increased to the machine limit. The far- and near-field influences are shown to be evaluated based on the same far-field approximation, but the near-field solution requires subdividing the panels into smaller subpanels continuously, which can be effectively implemented due to the B-spline representation of the geometry. A null pressure jump Kutta condition at the trailing edge is found to be effective in stabilizing the solution process and in predicting the correct solution. Numerical experiments indicate that the present method is robust and predicts the pressure distribution on the blade surface, including very close to the tip and trailing edge regions, with far fewer panels than existing low order panel methods.

B-스플라인 고차패널법에 의한 2차원 수중익 문제 해석 (Analysis of Two-dimensional Hydrofoil Problems Using Higher Order Panel Method based on B-Splines)

  • 조충호;김건도;이창섭
    • 대한조선학회논문집
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    • 제36권4호
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    • pp.9-20
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    • 1999
  • 기하학적 형상과 유동의 해를 B-스플라인으로 표현하는 2차원 고차 패널법이 개발되어 수중익 문제의 해석에 적용되었다. 제어점이 패널내에 놓이는 경우, 고차의 다이폴과 쏘오스에 의해 유기되는 자기 유기 포텐셜의 특이 거동을 제거하기 위하여 피적분 함수를 특이 부분과 비특이 부분으로 나누어, 특이 부분을 해석적인 적분으로 비특이 부분은 정도 높은 Gauss 구적법으로 계산함으로써 유기 포텐셜을 정도 높게 구할 수 있음을 보였다. 또한, 날개 뒷날에서의 압력 점프의 값이 명시적으로 영이 되도록하는 동역학적 Kutta 조건식을 도입하고, 이의 적용이 안정된 해를 보장함을 확인하였다. 수치 실험을 통하여, 제안된 수치해석 기법이 안정적이고 정확한 해를 줌을 확인하였으며, 특히 저차 패널법과 비교하여 적은 수의 패널로 동일한 정도를 유지할 수 있음을 보였다.

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2차원 B-스플라인 기저 고차패널법의 수치실험 (Numerical Experimentation of a 2-D B-Spline Higher Order Panel Method)

  • 조충호;이창섭
    • 대한조선학회논문집
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    • 제37권3호
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    • pp.27-36
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    • 2000
  • 기하학적 형상과 유동의 해를 B-스플라인으로 표현하는 2차원 고차 패널법이 개발되어 수중익 문제의 해석에 적용되었다. 기존의 Lee/Kerwin은 한 패널에 여러 개의 제어점을 배치하여 최소자승법에 의해 해를 구하였으나, 본 논문에서는 필요한 개수의 제어점 만을 표면에 규칙적으로 배열하여 해를 구할 수 있음을 수치 실험을 통하여 보였다. 특히, 날개 뒷날에서의 압력 점프의 값이 명시적으로 영이 되도록 하는 동역학적 Kutta 조건식의 도입이 중요하고, 이의 적용이 안정된 해를 보장함을 확인하였다. 해석해에 의해서 구해진 2차원 날개의 압력 분포와의 비교를 통하여, 적은 수의 제어점을 선정하여도 정확한 해를 얻을 수 있음을 보였으며, 동시에 계산속도도 현저하게 감소함을 보였다.

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