• Proceedings of the Computational Structural Engineering Institute Conference
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• 2009.04a
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• pp.255-258
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• 2009

본 논문에서는 최근 건축구조물의 보수보강에 사용되고 있는 복합재료보의 정확한 보강성능을 규명하기 위하여 다양한 실물 실험을 수행하였으며 실험 결과를 검토하여 실제 보강효과를 검증하였다. 콘크리트의 재료비선형을 고려할 수 있는 수치해석 기법으로 실험결과를 재현하여 보강효과를 수치해석적으로 검증하였으며 복합재료보를 이용하였을 경우 확보할 수 있는 보강효과에 대하여 연구하였다. 일반적인 철근콘크리트 구조물에 복합재료보를 이용하여 보강하였을 경우, 약 80% 내외의 하중 증가효과를 확보할 수 있었다. 또한 수치해석을 통하여 보강효과를 검토한 결과, 실물실험과 유사한 결과를 얻을 수 있었으며 복합재료보의 시공시 사용되는 전단연결재의 효과를 고려한다면 거의 동일한 결과를 얻을 수 있을 것으로 판단된다. 현재까지의 연구결과, 복합재료보를 이용하여 구조물을 보강한 경우, 취성이 증가하는 것으로 알려져있으나 추가적인 연구를 통하여 연성을 확보할 수 있는 복합재료보의 연구개발이 가능할 것으로 예상된다.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2004.05a
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• pp.57-57
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• 2004

복합재료는 단독재료로서는 가질 수 없는 높은 비강성, 비강도 등의 우수한 재료 특성을 가지고 있으므로 산업분야가 다양해지고 경량화를 요구함에 따라 우주/항공 방위 산업, 자동차, 스포츠 등의 여러 분야에 사용되어 지고 있으며, 현재 1 차 구조재로서의 연구가 활발히 진행되어 지고 있다 그러나 복합재료 보 이론의 경우 현재까지 얇은 복합재료 보의 거동에 관한 연구는 활발히 진행되어 왔으나, 아직 두꺼운 복합재료 보의 거동에 관한 이론의 정립은 미비한 상태이며 구조재로서의 복합재료 보를 적용하기 위해서는 두꺼운 복합재료보를 적용하기 위해서는 두꺼운 복합재료 보 이론 모델의 개발이 시급한 실정이다.(중략)

• Proceedings of the Korean Society For Composite Materials Conference
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• 2001.10a
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• pp.99-104
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• 2001

Thermally induced vibration response of solar array is investigated. The solar array model consists of composite thin walled beam and solar blanket, spreader bar. The composite thin walled beam incorporates a number of nonclassical effects of transverse shear, primary and secondary warping, rotary inertia and anisotropy of constituent materials. The solar blanket is a membrane subjected to uniform tension in the z direction. The spreader bar is a rigid member. A coupled thermal structure analysis that includes the effects of structural deformations on heating and temperature gradient is investigated. A stability criterion given in parameters for establishes the conditions for thermal flutter.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2001.05a
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• pp.399-406
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• 2001

Thermally induced vibration response of composite thin walled beams is investigated. The thin-walled beam model incorporates a number of nonclassical effects of transverse shear, primary and secondary warping, rotary inertia and anisotropy of constituent materials. Thermally induced vibration response characteristics of a composite thin walled beam exhibiting the circumferentially uniform system(CUS) configuration are exploited in connection with the structural bending-torsion coupling resulting from directional properties of fiber reinforced composite materials and from ply stacking sequence. A coupled thermal structure analysis that includes the effects of structural deformations on heating and temperature gradient is investigated.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2002.05a
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• pp.303-310
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• 2002

The bending vibration and thermal flutter instability of spacecraft booms modeled as circular thin-walled beams of closed cross-section and subjected to thermal radiation loading is investigated in this paper. Thermally induced vibration response characteristics of a composite thin walled beam exhibiting the circumferantially uniform system(CUS) configuration are exploited in connection with the structural flapwise bending-lagwise bending coupling resulting from directional properties of fiber reinforced composite materials and from ply stacking sequence. The numerical simulations display deflection time-history as a function of the ply-angle of fibers of the composite materials, damping factor, incident angle of solar heat flux, as well as the boundary of the thermal flutter instability domain. The adaptive control are provided by a system of piezoelectric devices whose sensing and actuating functions are combined and that an bonded or embedded into the host structure.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2000.06a
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• pp.1292-1297
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• 2000

For dynamic system under the external irregular disturbance, a performance of the controller designed by using of the 'Heo-stochastic control methodology' is investigated by simulations and experiments. MIMO Flexible cantilever beam, sticked with piezoceramics used as a sensor and actuator, under the irregular disturbance at bottom is modelled in physical domain. Dynamic moment equation about the system is derived through both the Ito's stochastic differential equation and Fokker-Planck-Kolmogoroff equation and also system's characteristics in stochastic domain is analyzed. In this study, the controller suppresses the amplitude of the system's moment response to the external disturbance. MIMO PI controller('Heo-stochastic MIMO PI controller') is designed in the stochastic domain and the response characteristics are investigated in the time domain