• 한국공간구조학회논문집
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• 제7권4호
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• pp.73-78
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• 2007

연약지반에서 측방 유동에 의해 주변 지반에 큰 변형을 일으키며 이로 인하여 말뚝기초에 손상을 입히게 된다. 이러한 경우 설치된 말뚝을 수동말뚝이라 하며 편재하중이 작용하게 되고 이로 인해 측방토압을 받게 되며 측방변위가 발생하여 상부구조물에 영향을 미치게 된다. 그러나 국내의 경우 이러한 말뚝과 교대 변위간의 관계에 대한 예측 및 메커니즘에 대한 연구가 부족한 실정이다. 본 연구에서는 교대이동에 대한 해석을 위해 입체, 판 및 프레임 요소를 복합적으로 해석할 수 있는 연성 3차원 유한요소해석 프로그램을 개발하였다. 개발된 연성해석 프로그램을 이용하여 연약지반상 형상비(두께-지름비, t/D비)를 변수로 한 교대강관파일의 변형특성을 명확히 하였다.

• Advances in aircraft and spacecraft science
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• 제1권2호
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• pp.233-251
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• 2014

Each aircraft have to be certified for a specified level of impact energy, for assuring the capability of a safe flight and landing after the impact against a bird at cruise speed. The aim of this research work was to define a scientific and methodological approach to the study of the birdstrike phenomenon against several windshield geometries. A series of numerical simulations have been performed using the explicit finite element solver code LS-Dyna, in order to estimate the windshield-surround structure capability to absorb the bird impact energy, safely and efficiently, according to EASA Certification Specifications 25.631 (2011). The research considers the results obtained about a parametric numerical analysis of a simplified, but realistic, square flat windshield model, as reported in the last work (Grimaldi et al. 2013), where this model was subjected to the impact of a 1.8 kg bird model at 155 m/s to estimate the sensitivity of the target geometry, the impact angle, and the plate curvature on the impact response of the windshield structure. Then on the basis of these results in this paper the topic is focused about the development of a numerical simulation on a complete aircraft windshield-surround model with an innovative configuration. Both simulations have used a FE-SPH coupled approach for the fluid-structure interaction. The main achievement of this research has been the collection of analysis and results obtained on both simplified realistic and complete model analysis, addressed to approach with gained confidence the birdstrike problem. Guidelines for setting up a certification test, together with a design proposal for a test article are an important result of such simulations.

• Structural Engineering and Mechanics
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• 제90권3호
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• pp.219-232
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• 2024

In current study, for the first time, Nonlinear Bending of a skew microplate made of a laminated composite strengthened with graphene nanosheets is investigated. A mixture of mechanical and thermal stresses is applied to the plate, and the reaction is analyzed using the First Shear Deformation Theory (FSDT). Since different percentages of graphene sheets are included in the multilayer structure of the composite, the characteristics of the composite are functionally graded throughout its thickness. Halpin-Tsai models are used to characterize mechanical qualities, whereas Schapery models are used to characterize thermal properties. The microplate's non-linear strain is first calculated by calculating the plate shear deformation and using the Green-Lagrange tensor and von Karman assumptions. Then the elements of the Couple and Cauchy stress tensors using the Modified Coupled Stress Theory (MCST) are derived. Next, using the Hamilton Principle, the microplate's governing equations and associated boundary conditions are calculated. The nonlinear differential equations are linearized by utilizing auxiliary variables in the nonlinear solution by applying the Frechet approach. The linearized equations are rectified via an iterative loop to precisely solve the problem. For this, the Differential Quadrature Method (DQM) is utilized, and the outcomes are shown for the basic support boundary condition. To ascertain the maximum values of microplate deflection for a range of circumstances-such as skew angles, volume fractions, configurations, temperatures, and length scales-a parametric analysis is carried out. To shed light on how the microplate behaves in these various circumstances, the resulting results are analyzed.

• Coupled systems mechanics
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• 제1권4호
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• pp.311-324
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• 2012

Previous investigations have demonstrated that strong earthquakes can cause severe damage or collapse to storage tanks. Theoretical studies by other researchers have shown that allowing the tank to uplift generally reduces the base shear and the base moment. This paper provides the necessary experimental confirmation of some of the numerical finding by other researchers. This paper reports on a series of experiments of a model tank containing water using a shake table. A comparison of the seismic behaviour of a fixed base system (tank with anchorage) and a system free to uplift (tank without anchorage) is considered. The six ground motions are scaled to the design spectrum provided by New Zealand Standard 1170.5 (2004) and a range of aspect ratios (height/radius) is considered. Measurements were made of the impulsive acceleration, the horizontal displacement of the top of the tank and uplift of the base plate. A preliminary comparison between the experimental results and the recommendations provided by the liquid storage tank design recommendations of the New Zealand Society for Earthquake Engineering is included. The measurement of anchorage forces required to avoid uplift under varying conditions will be discussed.

• 한국전자파학회지:전자파기술
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• 제6권2호
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• pp.19-26
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• 1995

광대역용 박판 전파흡수체의 설계에는 자성재료가 많이 사용되며, 주로 자성재료 박판의 이면에 금속판을 접착하여 만든다. 이 경우,6개의 변수를 포함하는 한개의 이론식에 의해 무반사 또는 보다 실용적인 99% 이상의 흡수(20dB 전파감소)가 가능한 전파흡수체의 형상과 재료 및 전자파 상수가 정의된다. 2여B 전파감소에 해당 하는 정합 경제값을 계산하기 위하여 Secant법을 적용하였으며, 전파흡수체 설계시 허용 가능한 재료 상수값의 범위를 구하기 위하여 Secant볍을 응용한 search algorithm을 개발하였다. 6개의 변수 모두에게 적용할 수 있 는 이 수치해석 방법에 의해 최소의 반복 계산으로 정확한 값을 효율적으로 구할 수 있었다.

• 대한기계학회논문집
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• 제18권10호
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• pp.2675-2685
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• 1994

A study has been conducted to provide the experimental information for the velocity and temperature profiles of steam-air mixutre and to investigate their roles on the film condensation with wavy interface. Saturated gas mixture of steam-air was made to flow through the nearly horizontal$(4.1^{\circ})$ square duct of 0.1m width and 1.56m length at atmospheric pressure, and was condensated on the bottom cold plate. The air mass fraction in the gas mixture was changed from zero(W =0, pure steam) to one(W =1, pure air), and the bulk velocity was varied from 2 to 4 m/s. Water film was injected concurrently to investigate the effect of wavy interface on the condensation. The velocity and temperature profiles were measured by LDA system and thermocouples along the three parameters ; air mass fraction, mixture velocity and film flow rate. The profiles moved toward the interface with increasing steam mass fraction, mixture velocity and film flow rate. The Prandtl and Schmidt numbers were near one in the present experimental range, however there was no complete similarity between the velocity and temperature profiles of gas mixture. And the heat transfer characteristics and interfacial structure were coupled with each other.

• Coupled systems mechanics
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• 제1권1호
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• pp.1-7
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• 2012

The problem of laterally loaded piles is particularly a complex soil-structure interaction problem. The flexural stresses developed due to the combined action of axial load and bending moment must be evaluated in a realistic and rational manner for safe and economical design of pile foundation. The paper reports the finite element analysis of pile groups. For this purpose simplified models along the lines similar to that suggested by Desai et al. (1981) are used for idealizing various elements of the foundation system. The pile is idealized one dimensional beam element, pile cap as two dimensional plate element and the soil as independent closely spaced linearly elastic springs. The analysis takes into consideration the effect of interaction between pile cap and soil underlying it. The pile group is considered to have been embedded in cohesive soil. The parametric study is carried out to examine the effect of pile spacing, pile diameter, number of piles and arrangement of pile on the responses of pile group. The responses considered include the displacement at top of pile group and bending moment in piles. The results obtained using the simplified approach of the F.E. analysis are further compared with the results of the complete 3-D F.E. analysis published earlier and fair agreement is observed in the either result.

• 한국강구조학회 논문집
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• 제20권4호
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• pp.505-517
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• 2008

휨지배 거동을 나타내는 세장한 이중강판합성벽의 비탄성 거동을 예측하기 위하여 비선형 수치해석 모델이 연구되었다. 수치해석의 편리를 위하여, 제안된 모델은 비교적 단순한 모델을 가지고 비탄성 거동을 근사적으로 예측할 수 있는 거시적 모델로 개발되었다. 휨지배 거동을 나타내는 벽체에 대해서는 다중평행요소 모델이 사용되었으며, 깊은 연결보의 전단거동을 위하여 X형 대각요소 모델이 사용되었다. 각 요소의 주기거동을 예측하기 위하여 콘크리트 및 강판 요소에 대한 간략화된 일축의 주기모델을 제안하였다. 제안된 해석모델은 1자형 및 T형 단일벽과 병렬벽에 적용하였으며, 그 결과는 기존의 실험결과와 비교되었다.

• 한국정보통신학회논문지
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• 제8권4호
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• pp.894-900
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• 2004

원편파용 마이크로스트립 안테나 소자들은 많은 형태가 있는데, 이것은 훌륭한 단위 방사기로 사용되었다. 원편파용 안테나의 이점은 송$.$수신시스템 사이에 엄격한 설정을 요구하지 않기 때문에 원편파용 프린트 안테나는 많은 위성과 이동무선시스템에 자주 사용되었다. 원편팍용 마이크로스트립 안테나의 3 dB 축비와 임피던스의 광대역을 실현하기 위해서 복잡한 급전구조와 3층의 패치 소자가 연구되었다. 본 논문은 원편파용 광대역 마이크로스트립 크로스 슬롯 어레이 안테나의 설계를 나타낸다. 제안한 안테나는 급전부인 마이크로스트립 라인과 원편파 발생을 위한 방사부인 크로스 슬롯으로 구성되어 있다. 광대역을 위해서 3충 구조가 고려되었고, 크로스 슬롯은 급전선과 전자기적 결합을 한다. 1소자 크로스 슬롯 안테나의 최적 파라미터가 모멘트 법에 의해 해석 및 설계되었다. 이러한 파라미터들은 방사소자들 사이의 상호결함을 고려한 어레이 안테나 설계에도 적용되었다. 제안한 안테나의 우현편파와 좌현편파는 비대칭 크로스 슬롯 구조와 슬롯 위치에 의해 쉽게 제어된다. 1소자와 15소자 크로스 슬롯 안테나에서 1 dB 이하의 축비와 안테나의 광대역 특성을 얻었다.

• Earthquakes and Structures
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• 제26권3호
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• pp.203-218
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• 2024

Beam-column joints in the frame structure are at high risk of brittle shear failure which would lead to significant residual deformation and even the collapse of the structure during an earthquake. In order to improve the damage issue and enhance the recoverability of the beam-column joints, a sector lead rubber damper (SLRD) has been developed. The SLRD can increase the bearing capacity and energy dissipation capacity, and also demonstrating recoverability of seismic performance following cyclic loading. In this paper, the hysteretic behavior of SLRD was experimentally investigated in terms of the regular hysteretic behavior, large deformation behavior and fatigue behavior. Furthermore, a parametric analysis was performed to study the influence of the primary design parameters on the hysteretic behavior of SLRD. The results show that SLRD resist the exerted loading through the shear capacity of both rubber parts coupled with the lead cores in the pre-yielding stage of lead cores. In the post-yielding phase, it is only the rubber parts of the SLRD that provide the shear capacity while the lead cores primarily dissipate the energy through shear deformation. The SLRD possesses a robust capacity for large deformation and can sustain hysteretic behavior when subjected to a loading rotation angle of 1/7 (equivalent to 200% shear strain of the rubber component). Furthermore, it demonstrates excellent fatigue resistance, with a degradation of critical behavior indices by no more than 15% in comparison to initial values even after 30 cycles. As for the designing practice of SLRD, it is recommended to adopt the double lead core scheme, along with a rubber material having the lowest possible shear modulus while meeting the desired bearing capacity and a thickness ratio of 0.4 to 0.5 for the thin steel plate.