• 한국지진공학회논문집
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• 제28권2호
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• pp.77-83
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• 2024

The design shear strength equations of RC shear walls have been developed based on their performance under in-plane (IP) loads, thereby failing to account for the potential performance degradation of shear strength when subjected to simultaneous out-of-plane (OOP) loading. Most of the previous experimental studies on RC walls have been conducted in one direction under quasi-static conditions, and due to the difficulty in experimental planning, there is a lack of research on cyclic loading and results under multi-axial loading conditions. During an earthquake, shear walls may yield earlier than their design strength or fail unexpectedly when subjected to multi-directional forces, deviating from their intended failure mode. In this paper, nonlinear analysis in finite element models was performed based on the results of cyclic loading experiments on reinforced concrete shear walls of auxiliary buildings. To investigate the reduction trend in IP shear capacity concerning the OOP load ratio, parametric analysis was conducted using the shear wall FEM. The analysis results showed that as the magnitude of the OOP load increased, the IP strength decreased, with a more significant effect observed as the size of the opening increased. Thus, the necessity to incorporate this strength reduction as a factor for the OOP load effect in the wall design strength equation should be discussed by performing various parametric studies.

• Steel and Composite Structures
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• 제2권2호
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• pp.99-112
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• 2002

The differential quadrature method (DQM) is a numerical technique of rather recent origin, which by its continually increasing applications in different problems of engineering, is a competing alternative to the conventional numerical techniques for the solution of initial and boundary value problems. The work of this paper concerns the application of the DQM in the area of the buckling of multi layered orthotropic composite plates with various boundary conditions the buckling of multi layered composite plates with constant and variable thickness under axial compressive static loading is considered. The effects of fiber orientation and boundary conditions on static behavior of composite plates are presented. The comparison of results from the present method and those obtained from NISA II software shows the accuracy and reliability of this method.

• 한국유체기계학회 논문집
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• 제14권6호
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• pp.96-101
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• 2011

Korea Aerospace Research Institute is performing 3 stage transonic axial compressor development program. This paper introduces design step of the compressor, the performance test results and its analysis. In the fore part of the paper, aerodynamic process of the 3 stage axial compressor is presented. To satisfy both of the mass flow and pressure rise, the compressor should rotate at a high rotational speed. Therefore the transonic flow field forms in the rotor stages and it is designed with a relatively high pressure rise per stage to satisfy its design target. The compressor stage consists of 3 stages, and the bulk pressure ratio is 2.5. The first stage is burdened with the highest pressure ratio and less pressure rises occur in the following stages. Also it is designed that tip Mach number of the first rotor row does not exceed 1.3, while the maximum relative Mach number in the rotor stage is between 1.3~1.4 to increase the compressor flow coefficient. The final design has been confirmed by iterating three dimensional CFD calculations to verify design target and some design intentions. In the latter part of the paper, its performance test processes and results are presented. The performance test result shows that the overall compressor performance targets; pressure ratio and efficiency are well achieved. The stator static pressure distributions show that the blade loading is gradually increasing from the downstream of the compressor.

• Steel and Composite Structures
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• 제51권2호
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• pp.173-183
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• 2024

This study investigates a new seismic retrofit system that utilizes rotational friction dampers and axial springs. The retrofit system involves a steel frame with rotational friction dampers (RFD) at beam-column joints and linear springs at the corners, providing energy dissipation and self-centering capabilities to existing structures. The axial spring acts as a self-centering mechanism that eliminates residual deformations, while the friction damper mitigates seismic damage. To evaluate the seismic performance of the proposed retrofit system, a series of cyclic loading tests were carried out on a steel beam-column subassembly equipped with the proposed devices. An analytical model was then developed to validate the experimental results. A performance point ratio (PPR) was presented to optimize the design parameters of the retrofit system, and a performance-based seismic design strategy was developed based on the PPR. The retrofit system's effectiveness and the presented performance-based design approach were evaluated through case study models, and the analysis results demonstrated that the developed retrofit system and the performance-based design procedure were effective in retrofitting structures for multi-level design objectives.

• Structural Engineering and Mechanics
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• 제17권3_4호
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• pp.357-378
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• 2004

Nonlinear dynamic analysis of a reinforced concrete (RC) frame under earthquake loading is performed in this paper on the basis of a hysteretic moment-curvature relation. Unlike previous analytical moment-curvature relations which take into account the flexural deformation only with the perfect-bond assumption, by introducing an equivalent flexural stiffness, the proposed relation considers the rigid-body-motion due to anchorage slip at the fixed end, which accounts for more than 50% of the total deformation. The advantage of the proposed relation, compared with both the layered section approach and the multi-component model, may be the ease of its application to a complex structure composed of many elements and on the reduction in calculation time and memory space. Describing the structural response more exactly becomes possible through the use of curved unloading and reloading branches inferred from the stress-strain relation of steel and consideration of the pinching effect caused by axial force. Finally, the applicability of the proposed model to the nonlinear dynamic analysis of RC structures is established through correlation studies between analytical and experimental results.

• 한국항공우주학회지
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• 제33권12호
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• pp.76-82
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• 2005

본 연구에서는 축류형 마이크로터빈의 단 수를 단 단에서부터 최대 6단까지 변경하면서 각 단에서의 공력특성을 측정하였다. 실험에 사용된 마이크로터빈은 터빈입구에서 유량계수가 2.0, 부하계수가 3.25이며 유로의 평균직경이 25.8mm인 소형 축류형 다단터빈이 적용되었다. 정익과 동익의 솔리디티는 0.67~0.75 범위의 값이 적용되었으며 입구에 일정한 질유량과 전압력으로 조정한 후에 터빈의 부하를 변경하면서 탈설계 영역에서의 공력특성을 측정하였다. 본 실험에서는 단 당 최대 2kW/kg/sec의 비출력이 얻어졌으나 단수의 증가에 따라 비출력의 증가폭은 다소 완화되었으며, 토오크의 경우는 단수가 증가되면서 낮은 회전수 영역에서는 토오크의 증가폭이 일정하나 높은 회전수영역에서는 토오크의 증가폭이 둔화되었다. 블레이드의 높이에 비하여 팁간격의 영향이 크므로 터빈의 효율은 낮으나 단 수의 증가에 따라 증가가 가능하다.

• 대한기계학회논문집A
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• 제23권6호
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• pp.1039-1047
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• 1999

It is necessary to evaluate the fatigue behavior of rail steel under the multi-axial stress state to assure the railway vehicle's safety. For this purpose, the stress analysis to investigate the crack initiation criteria, static failure and fatigue behavior under mixed-mode are performed. The stress analysis results show that the initiation of the transverse fissure depends on the maximum shear stress below the surface. For the mixed mode, the fatigue crack growth behavior which is represented by the projection crack length and comparative S.I.F, ${\Delta}K_v$, shows the more conservative results. Also, its rate is lower than that of the case of the mode I, and this difference decreases with increasing the stress ratio, R.

• Composites Research
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• 제12권2호
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• pp.53-61
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• 1999

복합재료의 파단식은 강도계수의 산정이 쉽고, 형상이 유연하며, 논리적인 단순성을 유지하기 위하여 각 파단모드와 하중조건을 고려하는 것이 바람직하다. 본 연구에서는 인장 및 비틀림의 이축하중에 대한 등가강도를 도입함으로써 새로운 파단식을 유도하였다. 이축 실험 결과는 등가이축강도가 cos($tan^{-1}R_b$)의 지수함수로 표현됨을 보였다. 이축하중의 파단강도는 일방향 인장강도 및 비틀림강도와 이축비의 함수로 예측할 수 있다. 실험 데이터의 산포성은 Weibull 분포함수와 등가이축강도 개념을 이용하여 분석하였다. 또한, 일방향 인장 및 비틀림 S-N 선도로부터 복합하중하의 S-N 선도를 구할 수 있는 피로해석법을 평면 응력 모델을 기반으로 개발하였다. 예측결과는 적층복합재료의 이축강도와 피로수명의 실험 데이터와 잘 일치하였다.

• 한국ITS학회 논문지
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• 제16권2호
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• pp.171-179
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• 2017

본 논문에서는 비행체 탑재용으로 안테나의 소영화를 위해 GPS용 적층형 폴디드 마이크로스트립 패치 안테나를 제안하였다. 기존의 소형화된 마이크로스트립 패치 안테나는 고비 유전율의 유전체를 이용한 소형화로 유전체 손실에 의해 대역폭이 작아지고 효율저하가 발생하게 된다. 제안된 안테나는 기존의 단점을 보완하는 소형화를 위해 먼저 Rogers사 TMM 10i(비유전율=9.8, 손실탄젠트=0.002) 유전체를 이용하였고, 다음으로 perturbation 효과를 적용시킨 방사소자를 유전체 표면에 폴디드 구조로 구현하였다. 이렇게 GPS $L_1$대역에서 설계된 안테나의 방사소자 크기는 $20.3mm{\times}19.93mm$를 가지며, 기본 반파장 마이크로스트립 패치 원편파 안테나보다 94.2% 소형화 특성을 얻었다. 또한 -10 dB 대역폭의 경우 32.3 MHz(2.05%), 3 dB 축비 대역폭의 경우 6.7 MHz(0.43%)로 측정되었다. 방사패턴 측정 결과 최대이득은 x축 편파에서 0.56 dBi, y축 편파에서 1.23 dBi을 얻었다.

• 한국지반공학회지:지반
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• 제8권3호
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• pp.5-12
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• 1992

본 논문은 모래지반에 박힌, 기하학적 특성과 설치방법이 서로 다른 모형말뚝의 극한상장지지력에 대한 연구이다. 기하학적 특성의 측면으로는 균일직편말뚝, 선단확대말뚝, 다층확대말뚝과 앵커플레이트가 시험되고 기일직경말뚝에 대한 말뚝설치방법이 극한지지력에 미치는 영향을 조사하기 위해 매설, ao입, 진동관입방법이 연구되었다. 실험결과에 의하면 기초가 상장력과 압축력을 받는 경우에는 선단확대 말뚝이, 오직 상장력에 대해서는 앵커플레이트가 가장 효과적이며, 또한 말뚝설치방법 및 타입 말뚝의 선단 모양은 상장지지목에 큰 영향을 준다는 것이 밝혀졌다.