• Proceeding of KASS Symposium
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• 2008.05a
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• pp.80-85
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• 2008

This paper investigate the structure instability properties of the shelled space frame structure. The large structure must have thin thickness for build the large space structure there fore structure instability review is important when we do structural design. The structure instability of the shelled structure accept it sensitively by varied conditions. This come to a nonlinear problem with be concomitant large deformation. In this study, it is compared unstable behavior according to lode and boundary condition of the shelled space frame structure through numerical method which considered geometrical nonlinear and grasped influence for the instability phenomenon and investigated the fundamental collapse mechanism.

• Journal of the KSME
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• v.33 no.7
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• pp.614-627
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• 1993

좌굴하기 쉬운 구조물을 설계할 때는 반드시 좌굴특성에 대한 어떤 직관을 가져야 한다. 이글의 목적은 셸 구조물이 비선형붕괴(nonlinear collapse), 분기좌굴(bifurcation buckling) 또는 이들 모드의 조합에 의해서 어떻게 좌굴될 것인가에 대한 감각을 전하는데 있다. 이 불안정에 대한 직관적 이해는 보강되고 여러 요소들로 조립되며 분지셸(branched shell)을 갖거나 복잡한 벽구 조를 갖는 실제 셸 구조물 등의 많은 예에 의해서 얻어질 수 있다. 이 글에서는 수식의 개발이 아니라 불안정의 예측에 주안점을 두고 있으며, 큰 처짐과 소성의 조합에 의해 발생되는 비선 형좌굴과 결함민감도가 특히 강조된다. 또한 최적화된 구조물의 국부 및 전체 불안정, 좌굴모드의 상호작용, 그리고 결함민감도(imperfection sensitivity) 등이 예시된다.

• Computational Structural Engineering
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• v.6 no.3
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• pp.45-48
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• 1993

일반적으로 구조설계 실무자들은 컴퓨터 프로그램을 통한 구조물 해석시, 구조물의 안정성 여부로 인하여 한두번쯤은 고민을 하였을 것이라 생각된다. 본문은 해석프로그램이 언제 "구조물이 불안정하다"는 메시지를 출력하게 되는지, 왜 이런 문제가 발생하게 되는지와 함께 어떻게 이러한 문제에 대처해야 하는지에 대하여 설명하는 것을 목적으로 하고 있다.

• Computational Structural Engineering
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• v.9 no.2
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• pp.23-27
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• 1996

오늘날 기술혁신 전쟁의 최전방에 대응하는 것이 불연속 및 불안정 문제를 포함하는 비선형문제이고, 비선형문제에도 도전하고 이를 극복하기 위한 최첨예 무기는 바로 컴퓨터라 할 수 있다. 그러나 인간이 본질인 시행착오를 생각해 보면, 오늘날 범람하고 있는 컴퓨터로부터의 출력 데이터는 매우 위험한 존재가 될 수도 있다. 본 고에서는 제3의 과학시대가 열린 오늘날, 범람하는 많은 컴퓨터 출력 데이터의 위험성을 자각하기 위해 돔형 쉘의 구조불안정 문제에 얽힌 재미있는 한 예를 설명하고, 이러한 오류에 대응하기 위한 검정방안을 제시한다.

• Journal of Korean Association for Spatial Structures
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• v.10 no.1
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• pp.119-126
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• 2010

The some papers which deal with the dynamic instability for shell-like structures under the dynamic excitation have been published, but there are few papers which treat the essential phenomenon of the dynamic buckling using the phase plane for investigating occurrence of chaos. In nonlinear dynamic, examining the characteristics of attractor on the phase plane and investigating the dynamic buckling process are very important thing for understanding why unstable phenomena are sensitively originated by various initial conditions. In this study, the direct and indirect snapping of shallow EP shell considering geometrical nonlinearity are investigated by Galerkin method numerically. This finding out the characteristic of the dynamic instability through the phases curves and running response spectrum.

• Journal of Korean Association for Spatial Structures
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• v.10 no.2
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• pp.95-103
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• 2010

This paper study on the accuracy improvement of nonlinear stiffness equation. The large structure must have thin thickness for build the large space structure there fore structure instability review is important when we do structural design. The structure instability of the shelled structure is accept it sensitively by varied conditions. This come to a nonlinear problem with be concomitant large deformation. Accuracy of nonlinear stiffness equation must improve to examine structure instability. In this study, space truss is analysis model Among tangent stiffness equation and nonlinear stiffness equation is using nonlinearity analysis program. The study compares an analysis result to investigate accuracy and convergence properties improvement of nonlinear stiffness equation.

• Journal of the Korean Society of Propulsion Engineers
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• v.16 no.5
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• pp.10-19
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• 2012

To eliminate the onset of combustion instabilities and develop effective approaches for control, flame structure is very important. In this study, we conducted experiments under various operating conditions with a model gas turbine combustor to examine the relation of combustion instability and flame structure by OH chemiluminescence and laser diagnostics of He-Ne laser absorbtion system. The swirling LNG($CH_4$)/air flame was investigated with overall equivalence ratio of 1.2 and dump plane fuel-air mixture velocity 25 ~ 70 m/s. We founded that the combustion instability phenomenon occurs at lower mixing velocity and higher mixing velocity conditions. We also concluded that fluid dynamical vortex frequency has major effects on the combustion instability characteristics at lower mixing velocity condition.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2012.05a
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• pp.367-376
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• 2012

To eliminate the onset of combustion instabilities and develop effective approaches for control, flame structure is very important. In this study, we conducted experiments under various operating conditions with a model gas turbine combustor to examine the relation of combustion instability and flame structure by OH chemiluminescence and laser diagnostics of He-Ne laser absorbtion system. The swirling LNG(CH4)/air flame was investigated with overall equivalence ratio of 1.2 and dump plane fuel-air mixture velocity 25 ~ 70 m/s. We founded that the combustion instability phenomenon occurs at lower mixing velocity and higher mixing velocity conditions. We also concluded that fluid dynamical vortex frequency has major effects on the combustion instability characteristics at lower mixing velocity condition.

• Journal of Korean Association for Spatial Structures
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• v.4 no.2 s.12
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• pp.63-71
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• 2004

The structural space is gradually wide and is wanting agreeable environment by the requirement and necessity of people who lives modem stage. The building coincides with such requirements and is the high rise building actual circumstances which is doing ultra-large. The confirmed report of the technology to organize great merit is becoming currently considerably important issue in constructing a building field. Thus, this paper examine closely for nonlinear unstable taking a picture uneasiness height of prosperity considering to initial imperfection by a numerical method with a space frame structure of discrete system in large space structure. Based on previous investigation method, this paper induce nodal stiffness matrix of solid truss elements considering geometrical nonlinear using finite element method. In this paper, three types of space structure considered; i) 1-free node space structure, ii) 2-free node space structure, iii) multi-free node space structure. It apply the above examples to a nonlinear program, next, grasp the characteristic of an unstable conduct and the result was a clearing low.

• Computational Structural Engineering
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• v.3 no.4
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• pp.14-23
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• 1990

구조물의 초기결함 민감도해석과 관련하여 카타스트로피 이론을 적용할 수 있는 가능성을 다음과 같이 요약할 수 있다. 첫째, 카타스트로피 이론은 현재까지 수행된 구조불안정현상의 분류에 대한 일반화된 수학적 근거를 제공해 준다. 둘째, 카타스트로피 이론에 의하면 구조물에서의 초기결함 민감도 특성을 위상수학적인 방법론에 의해 적은 계산량으로 구할 수 있다. 셋째, 복잡한 좌굴현상 예를 들면 Modal Interaction, Compound Buckling의 현상이 발생하는 경우 좌굴점근처에서의 분기특성, 초기결함 민감도 특성을 효과적으로 규명하는 모델로서 고차카타스트로피를 이용할 수 있다.