• 대한기계학회논문집A
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• 제36권3호
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• pp.305-311
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• 2012

보강 원통셸의 기본 고유 진동수를 최적화하기 위해서, 보강재의 개수를 1 개에서 5 개까지 보강된 원통셸에 대한 시뮬레이션을 수행하였다. 고유 진동수에 대한 최적화를 시뮬레이션하기 위해서 ANSYS 11.0 을 사용하였다. 최적화 방법으로 Subproblem Approximation Method 를 이용하였다. 최적화의 설계 함수로는 T-형 링 보강재의 기하형상이며, 제한 함수로는 보강에 따른 추가 부피가 10 % 이내로 제한하였다. 목적함수는 기본 고유진동수를 최대화하는 것이다. 최적 설계에 대한 성능 지표는 비보강 원통셸과 보강원통셸의 고유진동수와 부피의 비로서 정의하였다. 최적 성능 지수는 3 개의 보강재를 사용한 원통셸에서 나타났다.

• 한국구조물진단유지관리공학회 논문집
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• 제8권2호
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• pp.147-158
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• 2004

많은 장점을 가진 복합재료를 사용한 보강판에 대하여 지금까지 많은 연구자들이 변위법에 근거한 등매개변수 평판 요소와 보요소를 결합한 유한요소법을 사용하여왔다. 이러한 유한요소법은 보요소를 평판 요소의 절점에 대한 강성으로 치환하기 때문에 보강재에 대한 국부적인 거동을 파악할 수 없으며 복합적층 구조인 경우 그 적용성이 제한적이다. 따라서, 본 연구에서는 복합재료 보강판의 해석에 있어 보강재 및 판에 대하여 3차원 쉘요소를 사용하여 거동을 분석하고자 한다. 본 연구에서는 Reissner-Mindlin의 1차 전단변형이론을 사용하였다. 그러나 Reissner-Mindlin이론에 의한 등매개변수 평판 휨 요소는 판의 두께가 얇아지는 경우 일반적으로 전단잠김현상과 가상의 제로에너지 모드가 발생하는데 이를 제거하기 위해 대체전단변형률장을 사용하였다. 폭-두께비, 형상비 뿐만아니라 경사판의 경사각 변화에 따른 임의방향 보강재를 갖는 단순지지된 복합적층 구형 및 경사판에 대한 처짐분포를 비교 분석하였다.

• 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°.

• 대한기계학회논문집A
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• 제20권10호
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• pp.3199-3210
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• 1996

The buckling and postbuckling behaviors were sutdied analytically and experimentally for stiffened laminated composite panels under compression loading. The panels with I-, blade, -and hat-shapeed stiffeners were investigated. In the analysis, the stiffened panels were anlyzed using the nonlinear finite element method combined with an improved arc-length method. The progressive failure analysis was done by adopting the maximum stress criterion and complete unloading failure model. The effects of the fiber angles were investigated on the buckling and postbuckling behaviors. In the experiment, the web and the lower cap of each stiffener were formed by the continuous lay-up of the skin for cocuring the stiffened panels. Therefore, the separation between stiffener and skin was not found in the junction part even after postbuckling ultimate load and the stiffened panels had excellent postbuckling load carrying capacity. A shadow moire thchnique was used to monitor the out-of-plane deformations of the panels. The piezoelectric films were attached to the panels to get the failure characteristics of the panel. The analytical results on the buckling load, postbuckling ultimate load, and failure pattern showed good agreement with the experimental results.

• Structural Engineering and Mechanics
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• 제42권4호
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• pp.507-530
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• 2012

Age-related problems especially corrosion and fatigue are normally suffered by weatherworn ships and aging offshore structures. The effect of corrosion is one of the important factors in the Common Structural Rule (CSR) guideline of the ship design based on a 20 or 25 years design life. The aim of this research is the clarification of the corrosion effect on ultimate strength of stiffened panels on various types of double hull oil tankers. In the case of ships, corrosion is a phenomenon caused by the ambient environment and it has different characteristics depending on the parts involved. Extensive research considering these characteristic have already done by previous researchers. Based on this data, the ultimate strength behavior of stiffened panels for four double hull oil tankers such as VLCC, Suezmax, Aframax, and Panamax classes are compared and analyzed. By considering hogging and sagging bending moments, the stiffened panels of the deck, inner bottom and outer bottom located far away from neutral axis of ship are assessed. The results of this paper will be useful in evaluating the ultimate strength of an oil tanker subjected to corrosion. These results will be an informative example to check the effect of ultimate strength of a stiffened panel according to corrosion addition from CSR for a given type of ship.

• Steel and Composite Structures
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• 제32권4호
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• pp.479-495
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• 2019

In tied-arch bridges, the way the arch and the deck are connected may become crucial. The deck is usually suspended from hangers made out of steel pinned cables capable of resisting axial forces only. However, a proper structural response may be ensured by fixing and stiffening the hangers in order to resist, additionally, shear forces and bending moments. Thus, this paper studies the effect of different pinned and stiffened hanger arrangements on the structural behavior of the tied-arch bridges, with the intention of providing designers with useful tools at the early steps of design. Longitudinally and transversally stiffened hangers (and the effect of hinges at the hangers and their locations) are studied separately because the in-plane and the out-of-plane behavior of the bridge are uncoupled due to its symmetry. As a major conclusion, regarding the in-plane behavior, hangers composed of cables (either with vertical, $Nielsen-L\ddot{o}hse$ or network arrangements) are recommended due to its low cost and ease of erection. Alternatively, longitudinally stiffened hangers, fixed at both ends, can be used. Regarding the out-of-plane behavior, and in addition to three-dimensional arrangements of cables, of limited effectiveness, transversally stiffened hangers fixed at both ends are the most efficient arrangement. A configuration almost as efficient and, additionally, cheaper and easier to build can be achieved by locating a hinge at the end corresponding to the most flexible structural element (normally the arch). Its efficiency is further improved if the cross-section tapers from the fixed end to the pinned end.

• Steel and Composite Structures
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• 제51권5호
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• pp.543-562
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• 2024

While the external axial compressive load is applied to only the shell edge of stringer-stiffened shell in the most of numerical and analytical previous studies (entitled as conventional approach), a part of external load is applied to the stringers in real conditions. It leads to decrease the accuracy of the axial buckling load calculated by the conventional eigenvalue analysis approach performed in the most of previous studies. In this study, the distribution of stress in the pre-buckling analysis was enhanced by applying the axial external compressive load to both shell and stringers to perform an accurate eigenvalue analysis of the stringer-stiffened composite shell. In this regard, a model was developed in FORTRAN environment to simulate the laminated stringer-stiffened shell under axial compressive load using finite strip method. The axial buckling load of the shell was obtained through eigenvalue analysis. A comparison was made between the results obtained from the model and those available in the previous studies to evaluate the validity of the results obtained from the model. Through a parametric study, the effects of different parameters such as stringer properties and composite layup on the buckling load of the shell under different loading patterns were investigated. The results indicated that in some cases, the axial buckling load obtained for the conventional approach used in the most of previous studies is significantly overestimated or underestimated due to neglecting the stringer in distribution of external load applied to the stringer-stiffened shell. According to the results obtained from the parametric study, some graphs were derived to show the accuracy of the axial buckling load obtained from the conventional approach utilized in the literature.

• Composites Research
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• 제35권4호
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• pp.269-276
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• 2022

본 연구에서는 층간분리의 위험이 없는 3차원 직조방식으로 복합재 보강패널을 제작하고 좌굴하중과 고유진동수 등의 기계적 특성을 연구하였다. 보강패널의 스트링거와 외피는 일체형으로 제작하였고 T800급 탄소섬유로 만들어진 프리폼에 수지(EP2400)를 충진시키는 방식을 적용하였다. 제작된 보강판에 대하여 압축시험과 고유진동수 측정 시험을 수행하였고 유한요소해석 결과와 비교하였다. 또한 3차원 직조 구조물의 성능을 상대적으로 비교하기 위해 일방향 프리프레그와 2차원 평직(fabric)으로 동일한 치수의 보강패널을 제작하여 시험과 해석을 수행하였다. 시험값을 기준으로 일방향 프리프레그와 2차원 평직으로 제작된 보강패널의 좌굴하중은 3차원 직조 패널의 좌굴하중 대비 각각 20%, -3%의 차이를 보였다. 본 연구로부터 3차원 직조방식으로 제작된 일체형 보강패널의 좌굴하중은 일방향 프리프레그 적층 보강판의 좌굴하중보다는 낮지만 2차원 평직 보강판넬보다는 미세하게 높은 수준의 값을 보임을 확인하였다.

• 한국강구조학회 논문집
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• 제16권2호통권69호
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• pp.191-200
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• 2004

본 연구에서는 보강판을 직교이방성 판으로 해석하는 경우 보강판의 제원에 따라 정확도에 큰 차이를 보이는 단점을 해결하기 위하여, 개단면 리브를 갖는 보강판에 대하여 직교이방성 강성을 보정하는 방법을 제안하였다. 여러 가지 보강판에 대하여 등방성 및 직교이방성 판 요소로 모델링하여 해석하고 최대 처짐을 비교한 결과, 특정 강성비를 중심으로 이보다 강성비가 작아질수록 직교이방성 판이 더 작은 처짐을, 이보다 커질수록 더 큰 처짐을 나타내어 정확도의 향상을 위해서는 강성비에 따른 직교이방성 강성 수정이 이루어져야 함을 알 수 있었다. 거동 분석을 토대로, 직교이방성 판의 처짐식과 판만의 처짐과 관련한 처짐 비율을 이용하는 두 가지 강성 수정 방법을 제안하였으며, 두 경우 모두 오차율 및 오차율의 분포폭이 크게 감소하여 정확도가 크게 향상되지만, 처짐 비율의 방법이 처짐식을 이용한 방법보다 사용성 및 안정성 측면에서 더 적절한 것으로 나타났다. 또한, 개단면 리브를 갖는 보강판을 직교이방성 판으로 해석하는 경우, 본 연구에서 제안한 강성 수정 방법을 사용하여 보강판의 직교이방성 휨강성을 보정하게 되면, 상당한 정확성의 증가로 보강판에 대한 간편하고 타당한 결과를 얻을 수 있을 것으로 판단된다.

• 한국해양공학회:학술대회논문집
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• 한국해양공학회 2004년도 학술대회지
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• pp.408-413
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• 2004

High speed planning boats also have been required more and more the rational strength analysis and evaluation for the optimal structural design in respect of the structural lightness according to the high speed trend. Even though the suggestion of the simple type equation for the equivalent dynamic pressure is reasonable to design the scantling of ship structure conveniently, many research activities for more reasonable improvement of the simple design pressure, have been continued to suggest the more accurate equivalent static description of tire structural response such as the deflection and stress of hull structure. In this research, we focus on the aluminum bottom stiffened plate structure in which structural scantling is mainly depend on the local loads such as dynamic or impact pressure without other load effects and structural response for the simple dynamic equivalent pressure was investigated through the structural analysis. In order to investigate the structural response of the bottom stiffened plate structure subjected to the dynamic equivalent design pressure, linear and nonlinear structural analysis of the bottom stiffened plate structure of 4.3 ton aluminum planning boat was performed based on the equivalent static applied loads which were derived from the KR regulation and representative one among various dynamic equivalent pressure equations. From above analysis results, we found that the response such as deflection and stress of plate member was similar with the response results of one plate member model with fixed boundary, which was published previous paper and in case of KR design loading, all response of stiffened plate structure were within elastic limit. Through the nonlinear analysis, nearly elastic behavior including the slight geometrical nonlinear response was dominant but plastic local zone was appeared at $85\%$ limit load. Therefore, we can say that through tire linear and nonlinear analysis, this stiffened plate member has no structural strength problem based on the yield criteria in case within $60\%$ limit load except the other strength point of view such as the fatigue and buckling problem.