• Journal of Mechanical Science and Technology
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• 제20권5호
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• pp.658-667
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• 2006

Fractional derivative models, which are used to describe the viscoelastic behavior of material, have received considerable attention. Thus it is necessary to put forward the analysis solutions of dynamic systems containing a fractional derivative. Although previously reported such kind of fractional calculus-based constitutive models, it only handles the particularity of rational number in part, has great limitation by reason of only handling with particular rational number field. Simultaneously, the former study has great unreliability by reason of using the complementary error function which can't ensure uniform real number. In this paper, a new approach is proposed for an analytical scheme for dynamic system of a spring-mass-damper system of single-degree of freedom under general forcing conditions, whose damping is described by a fractional derivative of the order $0<{\alpha}<1$ which can be both irrational number and rational number. The new approach combines the fractional Green's function and Laplace transform of fractional derivative. Analytical examples of dynamic system under general forcing conditions obtained by means of this approach verify the feasibility very well with much higher reliability and universality.

• 한국항공우주학회지
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• 제35권1호
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• pp.40-45
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• 2007

구조물의 모달 해석 또는 모달 시험은 구조물의 동적 특성을 나타내는 모달 파라미터들을 구하는 과정이다. 모달 파라미터에는 고유 진동수, 감쇠율, 진동 모드의 세 가지 값들이 있다. 본 연구에서는 시스템의 개발과정에서 당연히 수행되는 모달 해석의 결과인 모달 파라미터를 활용하여 시스템 방정식을 구하는 방법에 대한 연구를 수행하였다. 상태 방정식의 고유치와 고유 벡터의 상관관계로부터 물리적 시스템 행렬인 질량, 감쇠, 강성 행렬을 각각 구하는 방법을 개발하였다. 간단한 질량-스프링-댐퍼 시스템과 외팔보에 대한 수치 예제를 통하여 개발된 방법의 유용성과 정확도를 검증하였다

• 대한기계학회논문집A
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• 제20권1호
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• pp.127-134
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• 1996

In general, seismic isolators which are made of laminated rubber and shim plate have characteristics of complex hysteretic behavior. When shear deformation of the seismic isolator is small, the isolator hassimple hysteretic almost bi-linear behabior. But on large shear deformation hardening effects may occur. This paper proposes a moldeling method of the seimic isolator with modified hysteretic bi-linear model which can consider the hardening effects. From the results of the seismic analyses of the isolated system it is shown that the responses are singificantly reduced compared with those of the non-isolated system. The modified hysteretic bi-linear model of the isolator gives larger ZPA(zero period acceleration) than those of the simple hysteretic bi-linear model and the equivalunt spring-damper model.

• 한국소음진동공학회논문집
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• 제17권12호
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• pp.1208-1216
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• 2007

Turbomachinery such as turbines, pumps and compressors, which are installed in transportation systems, including aircrafts, ships, and space vehicles, etc., often perform crucial missions and are exposed to potential dangerous impact environments such as base-transferred shock forces. To protect turbomachinery from excessive shock forces, it may be needed to accurately analyze transient responses of their rotors, considering the dynamics of mount designs to be applied. In this study a generalized FE transient response analysis model, introducing relative displacements, is proposed to accurately predict transient responses of a flexible rotor-bearing system with mount systems to base-transferred shock forces. In the transient analyses the state-space Newmark method of a direct time integration scheme is utilized, which is based on the average velocity concept. Results show that for the identical mount systems considered, the proposed FE-based detailed flexible rotor model yields more reduced transient vibration responses to the same shocks than a conventional simple model, obtained by treating a rotor as concentrated lumped mass, equivalent spring and a damper or Jeffcott rotor model. Hence, in order to design a rotor-bearing system with a more compact light-weighted mount system, preparing against any potential excessive shock, the proposed FE transient response analysis model herein is recommended.

• 한국소음진동공학회논문집
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• 제26권4호
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• pp.436-442
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• 2016

This paper presents the torsional vibration isolation performance evaluation of a centrifugal pendulum absorbers (CPAs) that has a continuously varying resonance frequencies proportional to engine firing (excitation) order. CPAs are commonly used to suppress torsional vibrations in rotating machinery and internal combustion engines. In this study, they are employed on the current spring type torsional damper inside a torque converter of automotive vehicle. To evaluate the effectiveness of designed resonance tuning order, the torsional vibration transmissibility based on torque measurements with respect to different engine firing orders is experimentally measured with a lower-inertia dynamometer. The torsional vibration transmissibility with respect to different frequencies with engine order of 2 is also evaluated. It has been demonstrated that the significant vibration reduction over operational frequency range of interest can be achieved by attaching simple pendulums. Future research direction includes the study on theoretical analysis, improved design of pendulum etc.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2003년도 추계학술대회논문집
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• pp.824-830
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• 2003

The Power Flow Finite Element Method(PFFEM) offers very promising results in predicting the vibration responses of system structures, and the first PFFEM software, PFADS has been developed in Seoul National University for the vibration predictions and analysis of coupled system structures in medium-to-high frequency ranges. PFFEM is numerical method which solves energy governing equation using finite element technique for complicated structures where the exact solutions are not available. Through the upgrades, the current version PFADS R3 could cover the general beam and plate structures including various kinds of beam-plate rigid joints, spring-damper connection and rigid body connection within beam and plate in addition. This software is composed of three parts; translator, model converter and solver. The translator makes its own FE-model from bulk data of commercial FE software, and the model converter is used to convert FE-model to PFFE-model automatically. The solver calculates vibrational energy density and intensity for PFFE-model by solving global matrix equations of PFFEM. For the applications of PFADS R3, two vehicle models and a container model are examined with respect to major parameters, and reliable results are obtained.

• 소음진동
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• 제5권1호
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• pp.107-115
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• 1995

드릴스트링의 종진동 해설을 위한 이론적 모델을 제시하였다. 드릴스트링은 균일봉들로 모델링하였으며, 비트와 바닥 암석과의 경계조건은 스프링과 댐퍼로 모델링하였다. 연결부(tool joint)의 영향, 드릴스트링 주위의 진흙물(mud)과 주변 암석의 영향등은 이론적으로 산정하였다. 비트에서의 경계조건을 산정하기 위하여, 드릴스트링의 종진동에 대한 강제진동 시험기법을 개발하여 실제의 드릴스트링에 대한 실험을 비트에 걸리는 힘(WOB)을 변화시키면서 수행하였다. 그 결과는 이론치 와 잘 일치함을 확인하였다. 본 연구결과 가장 중요한 결론은 드릴스티링의 종진동 해석에 있어서, 바닥 암석의 강성이 고려되어야 하며, 이 강성은 비트에 걸리는 힘의 크기에 따라 다르다는 것이다.

• 한국항공우주학회지
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• 제38권11호
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• pp.1130-1135
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• 2010

착륙장치는 완충장치를 이용하여 항공기 착륙 시의 충격을 흡수하는 역할을 한다. 다양한 종류의 완충장치가 존재하나, 완충효율 측면에서 가장 우수한 것은 유공압 방식이다. 착륙장치의 완충 성능은 반드시 낙하시험을 통해 입증하여야 하며, 이는 미 군사규격, 미연방 항공규정 등에서 공통적으로 요구하는 있는 사항이다. 이 논문에서는 낙하시험을 위한 설비 구성, 시험 절차 및 결과분석 방법을 실제 낙하시험 사례와 함께 제시한다.

• Journal of Ship and Ocean Technology
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• 제8권4호
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• pp.26-33
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• 2004

PFFEM software, PFADS has been developed for the vibration predictions and analysis of coupled system structures in medium-to-high frequency ranges. PFFEM is numerical method which solves energy governing equation using finite element technique for complicated structures where the exact solutions are not available. Through the upgrades, present PFADS R3 could cover the general beam and plate structures including various kinds of beam-plate rigid joints and other joint systems such as spring-damper junction and rigid bar connection. This software is composed of 3 parts; translator, model converter and solver. The translator makes its own FE-model from bulk data of commercial FE software, and the model converter is used to convert FE-model to PFFE-model automatically. The solver calculates vibrational energy density and intensity for PFFE-model by solving global matrix equations of PFFEM. For the applications of real transportation systems, a container ship model has been examined with respect to major parameters, and reliable results have been obtained.

• 대한조선학회논문집
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• 제33권4호
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• pp.87-96
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• 1996

평탄빙과 수직구조물이 상호작용 하는 경우의 구조물의 동적거동과 빙하중 추정을 하였다. 구조물의 형태는 수직구조물이고 얼음의 파괴형태는 분쇄파괴로 가정하였다. 평탄빙은 구조물과 접촉하여 분쇄파괴가 일어나는 접촉부위와 탄성변형을 하는 외곽부위로 나누었으며, 구조물은 스프링-질량-감쇄로 구성된 1자유도계로 치환하였다. 강성이 큰 구조물과 작은 구조물에 대하여 제시된 모델에 의한 계산결과와 실험결과를 비교하였다. 비교결과는 본 모델이 빙하중과 구조물의 거동추정을 정도있게 할 수 있다는 것을 보여주었다.