• Geomechanics and Engineering
• /
• 제36권3호
• /
• pp.277-293
• /
• 2024

Shored Mechanically Stabilized Earth (SMSE) walls are types of soil retaining structures that increase soil stability under static and dynamic loads. The damage caused by an earthquake can be determined by evaluating the probabilistic seismic response of SMSE walls. This study aimed to assess the seismic performance of SMSE walls and provide fragility curves for evaluating failure levels. The generated fragility curves can help to improve the seismic performance of these walls through assessing and controlling variables like backfill surface settlement, lateral deformation of facing, and permanent relocation of the wall. A parametric study was performed based on a non-linear elastoplastic constitutive model known as the hardening soil model with small-strain stiffness, HSsmall. The analyses were conducted using PLAXIS 2D, a Finite Element Method (FEM) program, under plane-strain conditions to study the effect of the number of geogrid layers and the axial stiffness of geogrids on the performance of SMSE walls. In this study, three areas of damage (minor, moderate, and severe) were observed and, in all cases, the wall has not completely entered the stage of destruction. For the base model (Model A), at the highest ground acceleration coefficient (1 g), in the moderate damage state, the fragility probability was 76%. These values were 62%, and 54%, respectively, by increasing the number of geogrids (Model B) and increasing the geogrid stiffness (Model C). Meanwhile, the fragility values were 99%, 98%, and 97%, respectively in the case of minor damage. Notably, the probability of complete destruction was zero percent in all models.

• International Journal of Aeronautical and Space Sciences
• /
• 제13권4호
• /
• pp.446-457
• /
• 2012

Aeroelastic analysis of an aircraft with a high aspect ratio wing for medium altitude and long endurance capability was attempted in this paper. In order to achieve such an objective, various structural models were adopted. The traditional approach has been based on a one-dimensional Euler-Bernoulli beam model. The structural analysis results of the present beam model were compared with those by the three-dimensional NASTRAN finite element model. In it, a taper ratio of 0.5 was applied; it was comprised of 21 ribs and 3 spars, and included two control surfaces. The relevant unsteady aerodynamic forces were obtained by using ZAERO, which is based on the doublet lattice method that considers flow compressibility. To obtain the unsteady aerodynamic force, the structural mode shapes and natural frequencies were transferred to ZAERO. Two types of unsteady aerodynamic forces were considered. The first was the unsteady aerodynamic forces which were based on the one-dimensional beam shape; the other was based on the three-dimensional FEM model shape. These two types of aerodynamic forces were compared, and applied to the foregoing flutter analysis. The ultimate goal of the present research is to analyze the possible interaction between the rigid-body degrees of freedom and the aeroelastic modes. This will be achieved after the development of a reliable nonlinear beam formulation that would validate the current results as well as enable a thorough investigation of the nonlinearity. Moreover, such analysis will allow for an examination of the above-mentioned interaction between the flight dynamics and aeroelastic modes with the inclusion of the rigid body degrees of freedom.

• 화약ㆍ발파
• /
• 제41권3호
• /
• pp.62-72
• /
• 2023

1970년대 산업화에 따른 플랜트 구조물이 노후화됨에 따라 구조적 기능을 상실해 발파 해체 공법을 활용한 해체 철거 수요가 증가하고 있다. 발파 해체공법은 기계식 해체공법에 비해 해체 공기가 짧아 환경공해 발생 노출 시간을 최소화할 수 있지만 잘못된 발파 설계 및 시공 계획에 따른 붕괴거동의 실패는 안전성에 매우 큰 위험을 유발한다. 따라서 붕괴거동 모사를 통해 최적의 발파 해체 조건과 이에 따른 영향을 고려하는 것이 중요하다. 본 연구에서는 Finite element method (FEM)와 Discrete element method (DEM)의 장점을 활용해 구축된 3-D Combined finite discrete element method (FDEM) 코드 기반 3-D DFPA 를 적용해 (구)서천화력발전소의 연돌 구조물에 대한 해체 모사를 수행하였으며 실제 구조물의 연돌 구조물 발파해체의 붕괴거동과 비교 분석하였다. 수치 모사 결과, 실제 구조물과 붕괴 거동 및 붕괴 완료 시간이 동일하게 나타났다. 또한, 발파구간 개구부 상부에 위치한 후드부의 크기가 연돌의 붕괴거동에 미치는 영향을 분석하기 위해 후드부의 면적을 조정하여 해체 모사를 수행하고 균열 발생 양상 및 z-방향 변위 곡선을 통해 비교 분석하였다. 분석 결과, 후드부의 면적이 증가함에 따라 하중을 지지하는 면적이 줄어들고 그에 따른 균열 발생 증가 및 전도 시간 감소를 확인하였다.

• Coupled systems mechanics
• /
• 제6권3호
• /
• pp.229-249
• /
• 2017

A new technique to mitigate irregular buildings with soil structure interaction (SSI) effect subjected to critical seismic waves is presented. The L-shape in plan irregular building for various reasons was selected, subjected to seismic a load which is a big problem for structural design especially without separation gap. The L-shape in plan building with different dimensions was chosen to study, with different rectangularity ratios and various soil kinds, to show the effect of the irregular building on the seismic response. A 3D building subjected to critical earthquake was analyzed by structural analysis program (SAP2000) fixed and with SSI (three types of soils were analyzed, soft, medium and hard soils) to find their effect on top displacement, base shear, and base torsion. The straining actions were appointed and the treatment of the effect of irregular shape under critical earthquake was made by using tuned mass damper (TMD) with different configurations with SSI and without. The study improve the success of using TMDs to mitigate the effect of critical earthquake on irregular building for both cases of study as fixed base and raft foundation (SSI) with different TMDs parameters and configurations. Torsion occurs when the L-shape in plan building subjected to earthquake which may be caused harmful damage. TMDs parameters which give the most effective efficiency in the earthquake duration must be defined, that will mitigate these effects. The parameters of TMDs were studied with structure for different rectangularity ratios and soil types, with different TMD configurations. Nonlinear time history analysis is carried out by SAP2000 with El Centro earthquake wave. The numerical results of the parametric study help in understanding the seismic behavior of L-shape in plan building with TMDs mitigation system.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2009년도 추계학술대회 논문집
• /
• pp.797-803
• /
• 2009

The accurate prediction of dynamic characteristics of high speed rotors, such as gas turbines, is important to avoid the possibility of operating the machinery near the critical speeds or unstable speed regions. However, the dynamic analysis methods and softwares for gas turbines have been developed in the process of producing many gas turbines by manufacturers and most of them have seldom been disclosed to the public. Recently, commercial FEM softwares, such as SAMCEF, ANSYS and NASTRAN, started supporting some rotordynamics analysis modules based on 3-D finite elements. In this paper, the dynamic analysis method using commercial S/W, especially ANSYS, is attempted for the small-size gas turbine engine rotor, and the analysis capability and limitations of its rotordyamics module are evaluated for further improvement of the module. As the preliminary procedure, the rotordyamic analysis capability of ANSYS was tested and evaluated with the reference models of the well-known dynamics. The limitations in application of the rotordynamics module were then identified. Under the current capability and limitations of ANSYS, it is shown that Lee diagram, a new frequency-speed diagram enhanced with the concept of $H{\infty}$ in rotating machinery, can be indirectly obtained from FRFs computed from harmonic response analysis of ANSYS. Finally, it is demonstrated based on the modeling and analysis method developed in the process of the S/W verification that the conventional Campbell diagram, Lee diagram, mode shapes and critical speeds of the small-size gas turbine engine rotor can be computed using the ANSYS rotordynamics module.

• 한국소음진동공학회논문집
• /
• 제20권1호
• /
• pp.36-44
• /
• 2010

The accurate prediction of dynamic characteristics of high speed rotors, such as gas turbines, is important to avoid the possibility of operating the machinery near the critical speeds or unstable speed regions. However, the dynamic analysis methods and softwares for gas turbines have been developed in the process of producing many gas turbines by manufacturers and most of them have seldom been disclosed to the public. Recently, commercial FEM softwares, such as SAMCEF, ANSYS and NASTRAN, started supporting some rotordynamics analysis modules based on 3-D finite elements. In this paper, the dynamic analysis method using commercial S/W, especially ANSYS, is attempted for the small-size gas turbine engine rotor, and the analysis capability and limitations of its rotordyamics module are evaluated for further improvement of the module. As the preliminary procedure, the rotordyamic analysis capability of ANSYS was tested and evaluated with the reference models of the well-known dynamics. The limitations in application of the rotordynamics module were then identified. Under the current capability and limitations of ANSYS, it is shown that Lee diagram, a new frequency-speed diagram enhanced with the concept of $H{\infty}$ in rotating machinery, can be indirectly obtained from FRFs computed from harmonic response analysis of ANSYS. Finally, it is demonstrated based on the modeling and analysis method developed in the process of the S/W verification that the conventional Campbell diagram, Lee diagram, mode shapes and critical speeds of the small-size gas turbine engine rotor can be computed using the ANSYS rotordynamics module.

• 한국지반공학회:학술대회논문집
• /
• 한국지반공학회 1988년도 학술세미나 강연집
• /
• pp.3-67
• /
• 1988

Model studies on the response of homgeneous earth embankment dams subjected to strike-slip fault movement have been penomed via centrifuge and finite element analysis. The centrifuge model tests have shown that crack development in earth embankment experiences two major patters: shear failure deep inside the embankment and tension failure near the surface. The shear rupture zone develops from the base level and propagates upward continuously in the transverse direction but allows no open leakage chnnel. The open tensile cracks develop near the surface of the embankment, but they disappear deep in the embankment. The functional relationship has been developed based on the results of the centrifuge model tests incorporating tile variables of amount of fault movement, embankment geometry, and crack propagation extent in earth des. This set of information can be used as a guide line to evaluate a "transient" safety of the duaged embankment subjected to strike-slip fault movement. The finite element analysis has supplemented the additional expluations on crack development behavior identified from the results of the centrifuge model tests. The bounding surface time-independent plasticity soil model was employed in the numerical analysis. Due to the assumption of continuum in the current version of the 3-D FEM code, the prediction of the soil structure response beyond the failure condition was not quantitatively accurate. However, the fundamental mechanism of crack development was qualitatively evaluated based on the stress analysis for the deformed soil elements of the damaged earth embankment. The tensile failure zone is identified when the minor principal stress of the deformed soil elements less than zero. The shear failure zone is identified when the stress state of the deformed soil elements is at the point where the critical state line intersects the bounding surface.g surface.

• 한국자동차공학회논문집
• /
• 제12권3호
• /
• pp.101-108
• /
• 2004

A FEM-based efficient method is developed for the shape optimization of 2-D structures. The combined SLP and Simplex method are coupled with finite element analysis. Selected set of master nodes on the design boundaries are employed as design variables and assigned to move towards their normal directions. The other nodes along the design boundaries are grouped into the master node. By interpolating the repositioned master nodes, the B-spline curves are formed so that the rest mid-nodes efficiently settle down on the B-spline curves. Mesh smoothing scheme is also applied for the nodes on the design boundary to maintain most finite elements in good quality. Finally, a numerical implementation of optimum design of an automobile torque converter piston subjected to pressure and centrifugal loads is presented. The results shows additional weight up to 13% may be saved after the shape optimization.

• 한국터널지하공간학회 논문집
• /
• 제20권3호
• /
• pp.543-560
• /
• 2018

도심지 지하공간의 개발과 운행선 하부를 저토피로 입체 교차화하는 시설 증가에 따라 비개착식 공법의 수요는 점차 증가추세에 있으나 대다수의 공법은 중대구경 강관을 압입하여 루프를 형성하고 내부를 굴착하는 파이프루프(Pipe roof) 계열의 공법이 주로 적용되고 있다. 강관 압입 시 발생되는 이완영역 및 하중은 여러 인자의 영향을 받게 되나 가장 큰 요소는 압입하는 강관의 크기에 좌우되며 이는 강관 루프 내 지중구조물에 작용하는 하중의 크기로 볼 수 있다. 지반의 교란 및 이완하중 발생을 최소화시키기 위해 개발된 SEM공법(Super Equilibrium Method)은 기존의 중대구경 강관 대신 ${\Phi}114mm$ 내외의 소구경 강관을 사용한다. 이 소구경 강관을 SEM파일로 명명하였으며 강관의 선 압입 및 그라우팅 보강을 실시한 후 지반의 침하나 융기 없이 지반 내 횡단구조물을 유압잭을 이용하여 압입하게 된다. 이와 같이 SEM공법의 구성 중 지보역할을 하는 SEM파일은 선단부 굴착 시 지반의 붕락을 방지하고 상재하중을 지지하기 위한 길이 5 m 내외의 Fore poling 파일이며 이 파일의 배치간격, 시공연장, 부재의 강성 등을 산정하기 위해서는 이완영역의 적절한 산정이 필수적이다. 본 논문은 SEM공법의 최적설계를 위하여 SEM파일 압입 시 발생되는 이완하중 산정 값을 비교분석하였다. 이완영역 산정에 근거한 주요 이론식 및 경험식들의 영향인자를 고려하여 분석하고 FEM analysis (유한요소 해석)를 수행하여 SEM파일에 적합한 이완하중 산정을 검토하였다. 또한 실제 SEM파일 압입 및 굴착 시 발생되는 지반이완을 확인하기 위해 강관압입 축소모형실험을 수행하였으며 토피고/강관(H/D)에 따른 지표침하 및 지반이완을 정량적으로 검토하였다.

• 소성∙가공
• /
• 제18권2호
• /
• pp.150-155
• /
• 2009

A shaft for laser printers has to be produced with high dimensional accuracy of a few micrometers. Most companies produce the shaft, therefore, by machining. These days, forging process is tried to be employed in manufacturing the shaft for productivity. In this study, the dimensional inaccuracy of straightness is studied and the underfill is not focused because the shaft shape is simple and the load capacity of press is sufficient. The straightness and concentricity of the shaft is important for the operation of a laser printer. Many design parameters such as preform shapes, tooling dimensions, forging load, and billet geometries may affect on the dimensional accuracy. In the forging process of shafts, a billet which is cut from wires is used. The billet, therefore, may be a little bit curved but not always straight. The elastic recovery is considered to cause the dimensional inaccuracy. Therefore, the effect of the forging load on the elastic recovery and straightness is investigated through the finite element analyses using DEFORM-3D and ABAQUS.