• Computational Structural Engineering
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• v.8 no.4
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• pp.129-136
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• 1995

This paper presents a boundary element method for obtaining approximate solutions of 2-dimensional consolidation problems based on the Biot's linear theory. Laplace transform is applied to differential equation system in order to eliminate the time dependency. The boundary integral equations in transformed space are formulated and the fundamental solutions are shown in a closed form. In order to convert the transformed solutions to the ones in real space, the Hosono's numerical Laplace transform inversion method is applied. As a numerical example, a half-space consolidation problem subjected to a strip local load is selected and the applicability of the method is demonstrated through the comparison with the exact solutions.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.11 no.3
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• pp.1-10
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• 1991

The paper is concerned with the analysis of laminated composite shell structures using an improved degenerated shell element. In the formulation of the element stiffness, the combined use of three different techniques was made. They are; 1) an enhanced interpolation of transverse shear strains in the natural coordinate system to overcome the shear locking problem; 2) the reduced integration technique in in-plane strains to avoid the membrane locking behavior; and 3) selective addition of the nonconforming displacement modes to improve the element performances. This element is free of serious shear/membrane locking problems and undesirable compatible/commutable spurious kinematic deformation modes. An incremental total Lagrangian formulation is presented which allows the calculation of arbitrarily large displacements. The resulting non-linear equilibrium equations are solved by the Newton-Raphson method. The versatility and accuracy of this improved degenerated shell element are demonstrated by solving several numerical examples.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1990.10a
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• pp.137-142
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• 1990

본 연구에서는 유한요소법을 사용하여 이방성으로 적층된 평판의 고유모드 를 예측하고, 이론적인 예측의 정확성을 연구하기 위해 사변 단순지지의 다 양한 각도로 적층된 정사각형 CFRP평판의 8번째 진동모드까지 실험적인 결 과와 비교하였다. 이 연구에서 사용된 모든 평판은 중앙면에 대칭이며, 이것 은 Bundling-stretching coupling을 제거하기 위해서이다. 그러나 만일 비대 칭적으로 적층된 평판이라면 이 효과를 포함한 해석이 되어야 할 것이다.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 1990.04a
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• pp.62-66
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• 1990

최근 미래지향적 첨단 산업 전반에 걸친 고부가가치 부품의 소재대체로 추진되고 있는 제 3의 소재 화인 세라믹스는 우수한 특성과 다양한 기능성으로 각광을 받고 있는 신소 재이나 고경도와 취성등으로 난삭재에 속한다. 화인 세라믹스는 제조법상 소결 공정을 필수로 하여그 수축현상을 피할 수 없으며, 고정도의 요소 부품화를 위해선 후가공을 필요로한다. 국내에선 일종의 세라믹스인 보석등의 미세구멍 가공등에만 국한되어 사용되어질뿐, 아직 화인 세라믹스의 형상 제거 가공등에는 그 가공법이 거의 적용되어 지지 않고 있는 초음파 가공에 대한 실험적 연구를 수행함으로써, 향후 최적 가공기술을 정립하는데 있어 지침이 되고자 한다.

• Proceedings of the Korean Society of Fisheries Technology Conference
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• 2000.10a
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• pp.213-214
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• 2000

총 암모니아성 질소(TAN)은 고밀도 양식에서 한계요소로 작용하는 수질인자 중의 하나이다. 생물학적 처리법에 의한 암모니아의 제거는 순환여과식 양식 시스템의 설계에서 가장 중요한 부분이다. 효율적인 순환 여과식 양식 시스템을 위해서는 생물반응기의 질산화 속도식을 구하여 적정한 용량의 처리시스템을 설계하여야 한다. (중략)

• Proceedings of the KIEE Conference
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• 2003.11a
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• pp.287-290
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• 2003

다모선 계통의 정확한 과도 안정도 직접해석을 위해 댐핑영향은 고려해야 할 중요한 요소 중의 하나이나 일반화가 어려워 최근까지 무시되어 왔다. 본 논문에서는 시스템을 나타내는 함수들의 적분 관계식들을 고려함으로써 다모선 계통에서의 댐핑영향을 반영한 에너지 함수를 유도하였으며 유도 과정에 있어 최근 다모선 계통에 보편적으로 적용되고 있는 관성중심(Center of Inertia :COI) 표현법으로 전개를 시도하였다. 유도된 에너지함수를 PEBS(Potential Energy Boundary Surface) 직접법에 적용하여 임계위치에너지를 산출하였으며, 임계고장제거시간을 계산함으로써 과도안정도직접해석법을 수행하였다. 제안된 에너지 함수를 WSCC 3기 9모선 샘플 시스템에 적용하여 댐핑이 고려된 에너지함수가 실제 계통을 보다 정확하게 표현하고 있음을 시뮬레이션을 통해 검증하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.37 no.5
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• pp.442-449
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• 2009

A two-dimensional cross-section analysis program based on the finite element method has been developed for composite blades with solid, thin-walled and compound cross-sections. The weighted-modulus method is introduced to determine the laminated composite material properties. The shear center and the torsion constant for any given section are calculated according to the Trefftz' definition and the St. Venant torsion theory, respectively. The singular value problem of cross-section stiffness properties faced during the section analysis has been solved by performing an eigenvalue analysis to remove the rigid body mode. Numerical results showing the accuracy of the program obtained for stiffness, offset and inertia properties are compared in this analysis. The current analysis results are validated with those obtained by commercial software and published data available in the literature and a good correlation has generally been achieved through a series of validation study.

• Magazine of the Korea Concrete Institute
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• v.7 no.3
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• pp.175-186
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• 1995

The determination of the stress intensity factors is investigated by sur-face integral method around the crack tip of the nlass~vc: concrete structure. The surface integral met hod is naturally derived from the standal-ci path integral J. Howevcr. In the J integral method, pressure in the crack-face and body forces can not be considered, while this theory has advantage of ccmsidering many kind of forces, so t.his theory will be useful in investigating more accurate strt:ss states around crack tip. Furthermore. t h~s rrlethod can elerninate unntussary process of using singular elements and fine mesh around crack tip which is used 11; modelling the singularity around crack tip. A computer program for determming $K_I$, $K_{II}$ is tfcvulopcd by applying this theory. $K_I$, $K_{II}$ values usmg X noded isoparametric elements which was proved and variation of the stress intensity factor was investigated by application of darn structures.

• Computational Structural Engineering
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• v.3 no.3
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• pp.113-123
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• 1990

The paper is concerned with the elasto-plastic and geometrically nonlinear analysis of shell structures using an improved degenerated shell element. In the formulation of the element stiffness, the combined use of three different techniques was made. They are; 1) an enhanced interpolation of transverse shear strains in the natural coordinate system to overcome the shear locking problem ; 2) the reduced integration technique in in-plane strains to avoid the membrane locking behavior ; and 3) selective addition of the nonconforming displacement modes to improve the element performances. This element is free of serious shear/membrane locking problems and undesirable compatible/commutable spurious kinematic deformation modes. In the formulation for plastic deformation, the concept of a layered element model is used and the material is assumed von Mises yield criterion. An incremental total Lagrangian formulation is presented which allows the calculation of arbitrarily large displacements and rotations. The resulting non-linear equilibrium equations are solved by the Netwon-Raphson method combined with load or displacement increment. The versatility and accuracy of this improved degenerated shell element are demonstrated by solving several numerical examples.

• Journal of the Korean Society of Propulsion Engineers
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• v.1 no.1
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• pp.104-110
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• 1997

To predict the effect of ring expansion and ring compression on residual stress relief of Al 7175 ring rot]s, 2-D axisymmetric thermal analysis and elastoplastic analysis were performed. The residual stress distributions along the thickness of T73, T7351 and T7352 treated rings were measured using three step sectioning method. The measured results were compared to numerical ones for quenched and stress relieved rings. After quenching, calculated hoop and axial residual stresses were similar to measured ones for T73 treated rings. The residual stresses of T7351 and T7352 treated rings were decreased remarkably compared to T73 treated rings. The effect of axial residual stress relief was superior to that of hoop one, and also ring compression to ring expansion. It was concluded that ring compression is advantageous over ring expansion in view of stress relief effect and practicality, and vice versa in view of dimensional control and press power.