• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.41 no.8
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• pp.619-624
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• 2013

To predict the probabilistic service life, statistical factors should be included to consider the uncertainty of parameters. Generally the probabilistic analysis is one of the common methods to account the uncertainty of parameters on the structural failure. In order to apply probabilistic analysis on the deterministic life analysis, it would be necessary to introduce Probability of Failure(PoF) and conduct risk assessment. In this work, we have studied probabilistic risk assessment of aircraft structures by using PoF approach. To achieve this goal, the Bayesian method was utilized to model PoF estimation since this method is known as the proper method to express the uncertainty of parameters. A series of proof tests were also conducted in order to verify the result of PoF estimation. The results from this efforts showed that the PoF estimation model can calculate quantitatively the value of PoF. Furthermore effectiveness of risk assessment approach for the aircraft structures was also demonstrated.

• Composites Research
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• v.19 no.3
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• pp.7-14
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• 2006

In this paper, an integrated probabilistic strength analysis was conducted to predict the reliability of a composite pressure vessel under inner pressure loading condition. As a probabilistic strength analysis, the probabilistic progressive failure model consisting of progressive failure model and Monte Carlo simulation was incorporated with a commercial FEA code, ABAQUS Standard, to perform the probabilistic failure analysis of composite structure which has a complex shape and boundary conditions. As design random variables, the laminar strengths of each direction were considered. Finally, from probabilistic strength analysis, the scattering of burst pressure could be explained and the reliability of composite pressure vessel could be obtained for each component. In case of composite structures in mass production, the effects of uncertainties in material and manufacturing on the performance of composite structures would apparently become larger. So, the probabilistic strength analysis is essential for the structural design of composite structures in mass production.

• Journal of Ocean Engineering and Technology
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• v.5 no.2
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• pp.85-93
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• 1991

피로 파괴연구의 급격한 발전에 따라 최근의 기계나 구조물들은 많은 분야에서 손상허용설계원리에 근거하여 설계되고 있다. 이러한 상황 하에서 피로파손의 정확한 특성을 밝히는 것은 신뢰성을 고려한 기계나 구조물의 설계에 있어 가장 중요한 요인이 된다. 피로파손은 많은 랜덤요소를 내포하고 있으므로 실험결과 분석 및 수명예측을 분석하기 위해서는 통계학적 해석이 요구되고 있다. 본 연구의 목적은 회전굽힘피로시험을 수행하고 피로수명을 분석하는데 정규분포, 대수분포, 지수분포 및 Weibull분포를 이용하여 실험결과와 비교하고 파손확률을 찾는데 있다.

• Magazine of the Korean Society of Agricultural Engineers
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• v.32 no.1
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• pp.7-16
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• 1990

불규칙파(不規則波)의 피습(被襲)에 의한 사석제(捨石堤)의 호안공(護岸工)이나 방파제(防波堤)에 대하여 화란(和蘭)이 Delft수이시험소(水理試驗所)에서 종합적(綜合的)인 모형연구(模型硏究)를 실시(實施)한 결과(結果) 새로운 안정도(安定度) 공식(公式)을 수립(樹立)하였다. 이들 공식(公式)은 파랑주기(波浪週期), 폭풍지속기간(暴風持續期間) 및 구조물(構造物) 투수성(透水性) 등의 파라미터(媒介變數)가 포함(包含)되어 있으므로 파손(破損)의 정도(程度)가 분명(分明)하여 Hudson형(型) 공식(公式)의 주(主)된 단점(短點)을 해결(解決)하였다. 이들 신공식(新公式)의 개발(開發)은 이전(以前)에도 기술(記述)된바 있으며 본론설(本論說)에는 재론(再論)하지 않는다. 안정도공식(安定度公式)은 파라미터로서 적용(適用)이 가능(可能)한 범위(範圍)가 부여(附與)되었으며, 이들 공식(公式)은 결정론(決定論) 및 확률론적(確率論的) 양자(兩者) 다같이 사용(使用) 방법(方法)이 제시(提示)되어 있다. 결정론적(決定論的) 설계절차(設計節次)는 여러가지지 파라미터의 영향(影響)을 곡선(曲線)으로 나타내어 졌으며 확률론적(確率論的) 설계(設計)는 구조물(構造物)의 내구연수기간내(耐久年數期間內)에 파손도(破損度)의 초과확률(超過確率)을 나타낸 곡선(曲線)으로 되어있다.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.26 no.3
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• pp.183-189
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• 2013

In this paper, uncertainties and failure criteria of structure are mathematically expressed by random variables and a limit state equation. A limit state equation is approximated by Fleishman's 3rd order polynomials and the theoretical moments of an approximated limit state equation are calculated. Fleishman introduced a 3rd order polynomial in terms of only standard normal distiribution random variables. But, in this paper, Fleishman's polynomial is extended to various random variables including beta, gamma, uniform distributions. Cumulants and a normalized limit state equation are used to calculate a theoretical moments of a limit state equation. A cumulative distribution function of a normalized limit state equation is approximated by a Pearson system.

• Journal of Ocean Engineering and Technology
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• v.2 no.1
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• pp.95-105
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• 1988

This paper describes the development of a reliability-based optimum design technique for such three dimensional tubular frames as off shore structures. The objective function is formulated for the structural weight. Constraints that probability of failure for the critical sections does not exceed the allowable probability of failure are set up. In the evaluation of the probability of failure, fatigue as well as buckling and plasticity failure are taken into account and the mean-value first-order second-moment method(MVFOSM) is applied for its calculation. In order to reduce the computing time required for the repeated structural analysis in the optimization process, reanalysis method is also applied. Application to two and three dimensional simple frame structures is performed. The influence of material properties, external forces, allowable failure probabilities and interaction between external forces on the optimum design is investigated.

• Journal of the Earthquake Engineering Society of Korea
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• v.13 no.6
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• pp.39-46
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• 2009

The selection of an evaluation response spectrum can have a significant effect on the seismic fragility evaluation of a structure. A method for modifying the seismic fragility parameters that are calculated based on the design spectrum is described in this study. The modification factor is used to modify the original fragility parameters. The HCLPF (High Confidence of Low Probability of Failure) acceleration levels of the electric system using previous design spectrum and uniform hazard spectrum (UHS) were compared. Finally, seismic risk analyses were performed according to a uniform hazard spectrum. From the results, it was concluded that based on the design spectrum, seismic risk for the electric system might be underestimated.

• Journal of Aerospace System Engineering
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• v.11 no.4
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• pp.1-7
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• 2017

The development of effective design allowable values for unmanned composite aircraft is an issue of paramount concern for the industry. The application of conventional manned aircraft structural certification methods to unmanned aircraft such as prototype and technology demonstrators, can lead to excessively long development time and costs. In this paper, the determining method of composite structure design allowable values for light composite unmanned aircraft is presented to reduce to the structural weight. This paper seeks to show the applicability of composite B-basis material values as a design allowable of light composite unmanned aircraft structures. A review of different civil and UAV targets failure probability is given. From the results, the researchers can know that the requirements of light composite unmanned aircraft design allowable should be alleviated, compared to manned composite aircrafts.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2004.05a
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• pp.78-78
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• 2004

기계 및 구조물의 설계시에는 허용응력 이하의 설계 조건으로 설계하지만 반복 작동을 하게 되는 기계 시스템의 경우에는 피로에 의한 파괴 현상이 나타나게 된다. 대부분의 기계 및 구조물은 사용시 변동 하중 상태에 놓이는 경우가 많게 되고 이로 인해 변동 응력이 작용되며 그 재료의 정적 강도보다 상당히 작은 간이라도 반복횟수가 증가함으로써 금속재료의 강도가 저하되어 결국 피로 파괴가 발생한다. 자동차, 항공기, 압축기, 펌프, 터빈 등과 같이 반복 작동을 하게 되는 기계 시스템에서 일어나는 파괴 현상 중에서 피로 파괴가 차지하는 비율이 점차 늘어나고 있다.(중략)

• Explosives and Blasting
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• v.37 no.4
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• pp.10-16
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• 2019

Information on overpressure, positive phase duration, and impulse are required to assess the effects of shock waves or pressure waves on the structure. In this study, the overpressure and positive phase duration were determined by applying the Multi-Energy Method, which is found to be effective in analyzing the explosion of vapor clouds. Based on the total heat of combustion estimated in the cyclohexane vapor cloud explosion in the Nypro Ltd(UK), overpressure and positive phase duration at the distance of 40, 80, 120, 160, 200, 240, 280, 320, 360(m) from the source of explosion were evaluated. Overpressure was shown to decrease exponentially and positive phase duration increased almost linearly with distance. A probit function was used to assess the probability of damages for the structures at each distance using the overpressure and impact obtained at the above mentioned distances. The Analyses of probability of damages have shown that there is a high probability of collapse at distances within 120m, major damage to structures within 240m, and minor damage and breakage of window panes of structures occur over the entire distances.