• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2010.05a
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• pp.552-553
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• 2010

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2010.05a
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• pp.154-155
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• 2010

• Journal of the Computational Structural Engineering Institute of Korea
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• v.15 no.1
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• pp.189-195
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• 2002

This paper deals with the free vibration of horizontally curved beams with transition currie. Based on the dynamic equilibrium equations of a curved beam element subjected to the stress resultants and inertia forces, the governing differential equations are derived for the out-of-plane vibration of curved beam with variable curvature. These equations are applied to the beam having transition curve in which the clothiod curve is chosen in this study. The differential equations are solved by the numerical methods lot calculating the natural frequencies and mode shapes. For verifying theories developed herein, the frequency parameters obtained from this studs and ADINA are compared with each other. As the numerical results, the various parametric studies effecting on natural frequencies are investigated and those results are presented in tables and figures.

• Journal of the Earthquake Engineering Society of Korea
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• v.14 no.2
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• pp.67-74
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• 2010

To a series of vibration records obtained from experimental modal testing using a fixed hammer and roving accelerometers for greenhouse arch structures, modal parameters such as natural frequencies, damping ratios and mode shapes are extracted by applying the two most advanced system identification methods in the frequency-domain up to now, so-called PolyMAX and FDD. The former involves both input and output data, while the latter utilizes only the output data. The possibility of determining the static buckling load, detecting damages, etc., for very slender steel-pipe arches by means of a non-destructive testing method based on vibration measurements is primarily investigated. The extracted modal parameters generally correlated well with those obtained using finite element analysis, demonstrating promising results for further on-going research.

• Proceedings of the Computational Structural Engineering Institute Conference
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• 2011.04a
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• pp.84-87
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• 2011

본 연구에서는 버페팅 해석을 통해 현수교 캣워크에 작용하는 풍하중에 대한 정적 및 동적 응답을 알아 보고 진동 억제 대책을 제시하였다. 캣워크는 영구구조물이 아닌 임시구조물이기 때문에 그동안 절적한 평가가 수행되지 못하였다. 따라서 본 연구는 풍하중에 의한 캣워크의 동적 응답을 해석적인 방법을 통해 알아보았으며, 동적 변위를 산정하기 위해 시간이력 해석 방법을 통해 버페팅 해석을 수행하였다. 그 결과로 부터 캣워크의 수평변위를 억제하기 위해 주케이블을 시공중에 연결하는 방법과 스테이 로프를 설치하는 방법을 제시하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.10
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• pp.919-926
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• 2011

The fin of high speed air vehicle is composed of skins and strong skeletons. In the flutter analysis, the eigenmodes of a fin are used for evaluating the unsteady aerodynamic force and the modal approach is applied for solving the flutter equation in both time and frequency domain. Therefore, the proper eigenmodes used for a modal flutter analysis should be chosen. For the appropriate choice of eigenmodes, when there exist local modes of a skin in the high modes, the effects of those modes on the unsteady aerodynamic force and flutter characteristics are anlalyzed.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2000.06a
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• pp.868-875
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• 2000

이 연구의 목적은 당사에서 제작한 멤브레인형 $130,000M^3$와 $135,000M^3$ LNG 운반선의 진동특성을 파악하고, 거주구역의 진동수준을 예측하기 위함이다. 우선 공진 회피의 관점에서 최적의 프로펠러를 선택하기 위해 간단한 계산을 수행한 후, 주변 해수를 고려한 선박 전체를 모델링하여 3차원 유한요소해석을 수행한다. 이 계산은 보다 정확한 고유진동수를 결정하고, 프로펠러 기진의 주파수 범위에서 관련된 모드 형상을 결정하며, 선박 거주구에서 기대되는 진동수준은 잘 예측할 수 있다. 다음으로 선박이 진수되고 전체구조가 조립된 후 안벽에서 불평형 가진기를 이용해 가진기테스트를 실시하고, 해상시운전 중에도 동일한 방법으로 테스트를 실시한다. 시험은 고유진동수의 항으로 선박의 실제진동응답과 계산결과와의 좋은 비교를 가능하게 한다. 추가적으로 실제 엔진을 구동해 RPM을 최저에서 최고까지 천천히 변경하면서 실제 운항 중 진동응답을 계측함으로서 고유진동수를 예측하여 해석결과 및 가진기 시험결과와 비교한다.

• Proceedings of the Korean Nuclear Society Conference
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• 1996.05c
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• pp.458-463
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• 1996

수송용기가 운반 트레일러에 의해 정상수송될 때, 국내 도로 상태에서 발생되는 반복적인 진동 흑은 충격하중을 측정하기 위해 국도 및 고속도로에서 차량수송시 가속도량를 기록하였으며, 이 측정결과를 주파수분석기로 분석하여 전산진동해석을 위한 입력자료를 생산하였다. 수송용기의 기계구조에 대한 건전성을 평가하기 위한 전산해석은 ABAQUS 코드로 KSC-7 수송용기를 3차원 보요소로 모델링하여 응력평가를 수행하였다.

• Journal of the Earthquake Engineering Society of Korea
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• v.16 no.3
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• pp.23-33
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• 2012

Dynamic response measurements from natural excitation were carried out for three 18-story office buildings to determine their inherent properties. The beam-column frame system was adopted as a typical structural form, but a core wall was added to resist the lateral force more effectively, resulting in a mixed configuration. To extract modal parameters such as natural frequencies, mode shapes and damping ratios from a series of vibration records at each floor, the most advanced operational system identification methods based on frequency- and time-domain like FDD, pLSCF and SSI were applied. Extracted frequencies and mode shapes from the different identification methods showed a greater consistency for three buildings, however the three lower frequencies extracted were 1.2 to 1.7 times as stiff as those obtained using the initial FE models. Comparing the extracted fundamental periods with those estimated from the code equations and FE analysis, the FE analysis results showed the most flexible behavior, and the most simple equation that considers the building height as the only parameter correlated fairly well with test results. It is recognized that such a discrepancy arises from the fact that the present tests exclude the stiffness decreasing factors like concrete cracking, while the FE models ignore the stiffness increasing factors, such as the contribution of non-structural elements and the actual material properties used.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.37 no.6
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• pp.586-594
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• 2009

This paper is the study on random, sinusoidal and shock vibration responses for the STSAT-3(science and technology satellite-3) proto-model which is the first small size all-composite satellite in Korea. The structure system of the STSAT-3 forms box type structure by joining several hybrid sandwich panels comprised of honeycomb core and carbon fiber reinforced laminated composite skins on both side. Mode shape, stress, displacement and acceleration responses are obtained on both the frequency domain and time domain by means of a commercial FEA software MSC/NASTRAN. From these analysis results, failure, safety factor and design validity are assessed. These results can be successfully applicable as reference data when a new satellite is developed as well as giving out an excellent criteria in satellite vibration treatment design.