• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2001.05a
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• pp.220-225
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• 2001

Asymmetric beams cause complicated vibration phenomena due to the inherent bending-torsion coupled vibration. In this paper, an exact dynamic element matrix for the bending-torsion coupled vibration of asymmetric beam is derived. An application of the derived exact dynamic element matrix is demonstrated by an illustrative example, wherein the natural frequencies by the proposed modeling method are compared with those available in the literature. Another numerical example is also illustrated which deals with a general beam with joints. The numerical study shows that the exact dynamic element model is useful for the dynamic analysis of asymmetric bending-torsion coupled beams.

• Journal of the Earthquake Engineering Society of Korea
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• v.5 no.1
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• pp.13-19
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• 2001

본 연구에서는 진동제어를 목적으로 강성이 비대칭적으로 분포된 구조물에 점탄성 감쇠기를 설치할 경우 비틀림 응답을 줄이기 위한 감쇠기의 효과적인 배치방법에 관하여 연구하였다. 비대칭 구조물의 응답에 미치는 점탄성 감쇠기의 효과를 알아보기 위하여 비대칭 비비례감쇠시스템의 특성방정식을 유도하고, 고유치해석을 통해 감쇠기가 설치된 비틀림 건물의 거동특성을 파악하였다. 이를 바탕으로 강성 편심 및 진동수비에 따른 최적 감쇠 편심을 찾아 이를 3차원 그래프로 나타내었다. 이를 이용하여 비대칭건물에 감쇠기를 설치했을 때 같은 양의 감쇠기를 대칭으로 설치하였을 때 보다 그 효과가 더욱 향상되는 것으로 나타났다. 또한 비대칭 건물의 비틀림제어면에서 점탄성 감쇠기가 점점 감쇠기보다 우수한 것으로 나타났다.

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.20 no.1
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• pp.10-21
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• 2010

Equations of chordwise and flapwise bending motions for the vibration analysis of rotating pre-twisted blades having tapered cross section and setting angle are derived by using hybrid deformation variable modeling. The two motions are couples to each other due to the pre-twisted angle of the beam cross section. The derived equations are transformed into dimensionless forms in which dimensionless parameters are identified. The effects of the dimensionless parameters on the modal characteristics of rotating pre-twisted blades having tapered cross section and orientation angle are investigated. The eigenvalue loci veering phenomena are also investigated and discussed in this work.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2009.04a
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• pp.288-295
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• 2009

Equations of chordwise and flapwise bending motions for the vibration analysis of rotating pre-twisted blades having tapered cross section and orientation angle are derived by using hybrid deformation variable modeling. The two motions are couples to each other due to the pre-twisted angle of the beam cross section. The derived equations are transformed into dimensionless forms in which dimensionless parameters are identified. The effects of the dimensionless parameters on the modal characteristics of rotating pre-twisted blades having tapered cross section and orientation angle are investigated. The eigenvalue loci veering phenomena is also investigated and discussed in this work.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.22 no.1
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• pp.190-197
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• 1998

Equations of motions of a pretwisted rotating blade with a concentrated mass in an arbitrary position are derived. The flapwise and chordwise equations are coupled to each other due to the pretwist angle of the blade. As the angular speed, hub radius ratio, pretwist angle and concentrated mass vary, the vibration characteristics of the blade change. It is found that eigenvalue lociveering phenomena occur between two closing loci due to the pretwist angle. The effect of the pretwist angle on the critical angular speed and location of the concentrated mass on the natural frequencies are also investigated.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.3
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• pp.14-21
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• 2006

The unsteady vortex lattice method is used to model twisting and flapping motions of a rectangular flat plate wing. The results for plunging and pitching motions were compared with the limited experimental results available and other numerical methods. They show that the method is capable of simulating many of the features of complex flapping flight. The lift, thrust and propulsive efficiency of a rectangular flat plate wing have been calculated for various twisting angles and reduced frequency with an amplitude of flapping angle($20^{\circ}$). And the effects of the twisting on the aerodynamic characteristics of the flapping wing are discussed by examination of their trends.

• Proceedings of the Acoustical Society of Korea Conference
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• 1998.06c
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• pp.299-302
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• 1998

가야금과 바이올린의 소리 발생 특성을 이해하기 위하여 모드해석을 수행하였다. 바이올린과 가야금은 크게 현과 몸체 그리고 이 둘을 연결하는 부분으로 구성되어 있다. 소리는 이들의 유기적인 관계로부터 발생된다. 실험을 통해 살펴본 결과, 저주파 대역에서 바이올린의 진동은 크게 앞, 뒷판의 진동, 몸체와 목 부분 사이의 비틀림 진동, 바이올린 전체가 하나의 보처럼 진동하는 현상으로 나누어 볼 수 있었다. 가야금 상판의 진동 형상은 약간 휘어진 형태를 가지며, 전체적으로 평판의 진동과 같은 모습을 보였다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1994.10a
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• pp.126-131
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• 1994

본 연구에서는 굽힘파(bending wave)의 전달만 고려하였는데 실제로는 보 및 비틀림 모드도 존재하나 고주파수 대역에서는 굽힘모드가 지배적이며 소음의 발생도 굽힘모드에 의해 주로 발생하므로 보 및 비틀림모드의 생략이 큰 오차를 가져오지는 않는다. 테스트 모델에 대해 실험을 수행하여 결과를 비교하였다. 또한 구조물의 고주파수 진동소음 해석방법으로 널리 쓰이는 통계적 에너지 해석법(SEA)을 이용한 결과와 비교하였다.

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.15 no.12 s.105
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• pp.1416-1421
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• 2005

This paper presents an analytical approach for the vibration characteristics of a piezoelectric disc for torsional vibration transducers. The characteristic equation of the piezoelectric annular disc has been derived from Gibbs' free energy equations and mechanical and electrical equilibrium. With an anisotropic material properties of the disc, the characteristic equation has yielded resonance frequencies. Numerically-calculated results have been compared with the results obtained by the finite element analysis and experiments and have confirmed the validity of the theoretical analysis.

• Proceedings of the Korean Society of Machine Tool Engineers Conference
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• 2002.10a
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• pp.153-157
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• 2002

본 연구에서는 선반가공에서 일반적인 선반작업 후 밀링이나 드릴링 가공이 가능한 복합가공기의 역할을 한번에 수행할 수 있는 CNC 공구터렛의 홀더 주축에 대한 수학적 모델링을 통하여 시스템의 횡진동 및 비틀림 진동 해석으로 발생할 수 있는 진동 문제에 대처할 수 있는 방안을 제시 하고자 한다.