• 대한기계학회논문집A
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• 제21권11호
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• pp.1931-1942
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• 1997

A new load/displacement parameter method is developed for the cases that loads are applied to one or more points, and displacements of a structure are controlled at one or more points sinultaneously. The procedure exploits a generalized Riks method, which utilizes load/displacement parameters as scaling factors in order to analyze the post-buckling phenomena including snap-through or snap-back. A convergence characteristic is improved by employing new relaxation factors in incremental displacement parameter, particularly at the region where exhibits severe numerical instability. The improved performance is illustrated by means of numerical example.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2005년도 추계학술발표대회 논문집
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• pp.280-284
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• 2005

Existing construction materials such as concrete and steel have chronic problems; deterioration and corrosion. Owing to its special features of light weight ‘ high durability, anti-corrosion, composite material used in civil infrastructure can not only solve fundamental problems of deterioration and corrosion, but also reduce both construction and maintenance cost significantly. After the fabrication of deck panel with snap-fit connection by pultrusion through composite design according to stacking sequence of composite laminates and structural analysis, performance of decks will be verified and evaluated by structural tests.

• 한국산학기술학회논문지
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• 제2권2호
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• pp.1-5
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• 2001

스냅핏은 일종의 결속장치로서 흔히 플라스틱 부품들을 서로 체결하는데 이용되는데, 다른 결속장치에 비해 간편하고. 생산품의 조립단가를 줄일 수 있고, 또한 분리력은 큰 반면에 결합력은 작게 만들 수 있는 장점을 가지고 있어 널리 사용된다. 스냅핏의 설계는 재료에 따른 물성(property) 및 구조적 강성(stiffness)이 설계 초기단계에서 고려되어야 하고, 또한 사출성형공정에서 스냅핏의 성형성도 예측되어야 한다. 그러나 스냅핏의 형상, 치수, 위치 등을 적절히 설계합성(synthesis)하고 적절한 재료를 선택하는 작업은 공정에 관한 종합적인 지식을 지원해 주는 합리적인 설계도구가 제공되지 못했던 이유로 사출 전문가의 오랜 기간 축적된 경험과 지식에만 전적으로 의존하여 왔다. 본 연구에서는 기존의 전문가에 의존해온 스냅핏 설계방법을 개선하기 위해 사출 성형에 의해 제한되어지는 지식을 규칙베이스화하고 재료의 물성과 스냅핏의 형상 및 치수에 따라 스냅핏이 갖는 결합력 분리력 변형하중 및 허용언더컷 등을 출력하는 설계 프로그램을 제안하였다.

• 한국군사과학기술학회지
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• 제23권6호
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• pp.533-541
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• 2020

This study using ABAQUS investigates the nonlinear vibration responses when thermal and random acoustic loads are applied simultaneously to the stiffened composite panels. The nonlinear vibration analyses are performed with changing the number of stiffeners, and layup condition of the skin panel. The panel and stiffeners both are modeled using shell elements. Thermal load (ΔT) is assumed to have the temperature gradient through the thickness direction of the stiffened composite panel. The random acoustic load is represented as stationary white-Gaussian random pressure with zero mean and uniform magnitude over the panels. The thermal postbuckling analysis is conducted using RIKS method, and the nonlinear dynamic analysis is performed using Hilber-HughesTaylor time integration method. When ΔT = 25.18 ℃ and SPL = 105 dB are applied to the stiffened composite panel, the effect of the number of stiffener is investigated, and the snap-through responses are observed for composite panels without stiffeners and with 1 and 3 stiffeners. For investigation of the effect of layup condition of the skin panel, when ΔT = 38.53 ℃ and SPL = 110 dB are applied to the stiffened composite panel, the snap-through responses are shown when the fiber angle of the skin panel is 0°, 30°, and 60°.

• 대한토목학회논문집
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• 제28권2A호
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• pp.187-196
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• 2008

이 연구에서는 단순 트러스 모델을 이용한 철근콘크리트 바닥판의 펀칭전단강도 평가방안을 제안하였다. 철근콘크리트 바닥판의 펀칭전단 해석의 본질적인 어려움을 극복하기 위해 집중하중이 작용하는 바닥판을 펀칭전단 파괴 형태에 기초하여 펀칭콘과 나머지 부분의 소구조체로 구분하였다. 펀칭콘의 강도는 이상화한 트러스의 경사압축부재의 강성도로써 유도되었다. 수평변위를 제어하고 있는 롤러지점의 수평방향 스프링 부재의 강성도는 펀칭콘 내에 포함된 철근에 의하여 결정되었다. 3차원 구조물의 2차원화에 따른 오차와 해석과정에 포함되지 않은 나머지 소구조체의 강성도 등에 기인하는 불확실성들을 포함하기 위하여 경사압축재의 초기각은 실험결과들에 대해 주인장 철근비를 변수로 수행된 회귀분석을 통하여 구하였다. 단순 트러스 모델로부터 구한 펀칭전단강도는 실험결과와의 비교에서 신뢰성이 높은 것으로 나타났다. 단순 트러스 모델의 스냅스로우(snap-through)좌굴해석으로부터 구한 펀칭전단강도는 철근콘크리트 바닥판의 펀칭전단강도의 검토에 유용하게 사용될 수 있을 것이다.

• 한국전산구조공학회논문집
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• 제12권3호
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• pp.407-415
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• 1999

쉘형 구조물의 불안정 현상은 크게 뜀좌굴과 분기좌굴로 분류할 수 있다. 이들은 구조물의 형상특성, 특히 형상 초기불완전에 대해 매우 민감하게 반응한다. 본 연구에서는, 형상 초기불완전을 가진 쉘형 구조물의 불안정 거동을 파악하기 위해 양단이 힌지로 고정된 얕은 정현형 아치의 평형경로를 조사한다. 비선형 방정식을 얻기 위해 Galerkin법을 이용하였으며, 증분형 방정식으로의 변환은 섭동법을 이용하였다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2006년도 추계학술대회논문집
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• pp.235-238
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• 2006

For high-speed aircraft and high-speed civil transport planes, certain structural skin components are subjected to very large acoustic loads in an elevated thermal environment. In this study, we used the single-mode Fokker-Panck distribution to predict displacements of isotropic plates subject to thermo-acoustic combined load. The single mode was formulated to predict the nonlinear dynamic responses of postbuckled plates under acoustic random excitation. Acoustic random excitation was used with Gauss distribution. Some important effects of the snap-through motion on the dynamic responses of the postbuckled plates are described.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 추계학술대회논문집A
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• pp.420-425
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• 2000

The room-temperature shapes of cured unsymmetric composite laminates have out-of-plane warping after autoclave processing. In addition, they exhibit two stable room-temperature configurations due to snap-through phenomena when the side length of laminates exceeds a critical value. The cured shapes of unsymmetric laminates are influenced by many environmental factors. Experiments show that the effect of too-plate cannot be ignored and has significant influence on the cured shape of unsymmetric laminates. In this present study, approximations to the strain fields are used in the expression for the total potential energy and the Rayleigh-Ritz method is applied. The slippage effects resulting from the interaction between the laminates and the tool-plate are considered. By introducing a dimensionless slippage coefficient and correlating the corresponding value with experimental results, the influence of processing parameters is investigated. Modeling is extended to predict curvatures of plate configurations with various aspect ratio.

• 제어로봇시스템학회논문지
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• 제18권3호
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• pp.168-174
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• 2012

This paper presents a bending propagating actuation using SMA (Shape Memory Alloy) spring for an effective shape transition of a flytrap-inspired soft morphing structure. The flytrap-inspired soft morphing structure is made from unsymmetric CFRP (Carbon Fiber Reinforced Prepreg) structure which shows bi-stability and snap-through phenomenon. For a thin and large curved bistable CFRP structure, SMA spring is more acceptable than SMA wire and piezoelectric actuator which used in previous investigations. A bending propagating actuation is proposed which can induce snap-through of the bi-stable CFRP structure effectively. From this research, effective shape transition of soft morphing structure is possible.

• Structural Engineering and Mechanics
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• 제36권5호
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• pp.529-544
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• 2010

Nonlinear equations of structures are generally solved numerically by the iterative solution of linear equations. However, this iterative procedure diverges when the tangent stiffness is ill-conditioned which occurs near limit points. In other words, a major challenge with simple iterative methods is failure caused by a singular or near singular Jacobian matrix. In this paper, using the Newton-Raphson algorithm based on Davidenko's equations, the iterations can traverse the limit point without difficulty. It is argued that the propose algorithm may be both more computationally efficient and more robust compared to the other algorithm when tracing path through severe nonlinearities such as those associated with structural collapse. Two frames are analyzed using the proposed algorithm and the results are compared with the previous methods. The ability of the proposed method, particularly for tracing the limit points, is demonstrated by those numerical examples.