• 대한기계학회논문집
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• 제17권5호
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• pp.1138-1149
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• 1993

본 연구에서는 임의 형태의 경계조건을 갖는 부분구조 모드를 이용하여 구조물의 고유치해석을 수행할 수 있는 새로운 혼합경계합성법을 제시한다. 각 부분 구조의 모드특성으로는 기존의 고정, 자유, 그리고 하중경계모드가 모두 사용될 수 있으며 고정 및 하중경계모드를 사용한 경우에는 두번의 연속적인 모드변환식이 사용 된다. 부분구조간의 연결부에서 정의되는 경계자유도만을 이용하여 고유치해석을 수행하며 고유치해석의 최종적인 특성방정식은 경계자유도의 갯수와 같은 연립방정식 에서 비롯되는 다항식이 된다. 제시한 방법은 유한요소법 뿐만 아니라 실험적 모드 해석을 통해 모형화된 부분구조를 쉽게 고려할 수 있는 장점이 있다. 제시한 방법을 간단한 집중질량계에 적용하여 부분구조모드의 특성과 수렴성 및 최적의 부분구조 모 드의 조합이 존재함을 보인다.

• International Journal of Aeronautical and Space Sciences
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• 제15권2호
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• pp.113-122
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• 2014

The objective of the paper is to clarify a methodology based on the use of the existing component mode synthesis methods for the case of two damped substructures which are coupled through a linking viscoelastic flexible substructure and for which the structural modes with free geometrical interface are used for each main substructure. The proposed methodology corresponds to a convenient alternative to the direct use either of the Craig-Bampton method applied to the three substructures (using the fixed geometric interface modes) or of the flexibility residual approaches initiated by MacNeal (using the free geometric interface modes). In opposite to a geometrical interface which is a topological interface on which there is a direct linkage between the degrees of freedom of substructures, we consider a physical flexible interface which exists in certain present technologies and for which the general framework linear viscoelasticity is used and yields a frequency-dependent damping and stiffness matrices of the physical flexible interface.

• 대한기계학회논문집
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• 제17권10호
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• pp.2457-2466
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• 1993

A simple method is presented for determining transient responses of locally nonlinear structures using substructure eigenproperties and Lagrange multiplier technique. Although the method is based upon the mode synthesis formulation procedure, the equations of the combined whole structure are not constructed compared with the conventional methods. Lagrange multi-pliers are used to enforce the conditions of geometric compatibility between the substructure interfaces and they are treated as external forces on each substructure itself. Substructure eigenvalue problem is defined with the substructure interface free of fixed. The transient analysis is based upon the recurrence discrete-time state equations and offers the simplicity of the Euler integration method without requiring small time increment and iterative solution procedure. Numerical examples reveal that the method is very accurated and efficient in calculating transient responses compared with the direct numerical integration method.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2000년도 춘계학술대회논문집
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• pp.536-542
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• 2000

The present paper introduces a new fixed interface component mode synthesizing technique based on the notion of higher-order field-consistency. The present technique employs higher-order residual constraint modes in addition to lower fixed interface normal modes while consistency in matching field variables at the substructure interface is maintained. The present field-consistency approach does not increase the size of the synthesized system even if higher-order residual constraint modes are included. A new field-consistent higher-order synthesis technique is first presented and a numerical example is given to verify the present method.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 1993년도 춘계학술대회논문집; 한국과학연구소, 21 May 1993
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• pp.52-56
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• 1993

An efficient method is presented for determining transient responses of locally nonlinear structures using substructure eigenproperties and Lagrange multiplier technique. The method is based upon the mode synthesis formulation procedure, but does not construct the equations of motion of the combined whole structure compared with the conventional methods. For modal bases of each linear substructure, either fixed or free interface modes can be employed. The transient analysis is based upon the recurrence discrete-time state equations and offers the simplicity of the Euler integration method without requiring small time increment and iterative solution procedure. Numerical examples reveal that the method is very accurate and efficient in calculating transient responses compared with the direct numerical integration method.

• Structural Engineering and Mechanics
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• 제39권1호
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• pp.47-75
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• 2011

An accurate substructural synthesis method including random responses synthesis, frequency-response functions synthesis and mid-order modes synthesis is developed based on rigorous substructure description, dynamic condensation and coupling. An entire structure can firstly be divided into several substructures according to different functions, geometric and dynamic characteristics. Substructural displacements are expressed exactly by retained mid-order fixed-interfacial normal modes and residual constraint modes. Substructural interfacial degree-of-freedoms are eliminated by interfacial displacements compatibility and forces equilibrium between adjacent substructures. Then substructural mode vibration equations are coupled to form an exact-condensed synthesized structure equation, from which structural mid-order modes are calculated accurately. Furthermore, substructural frequency-response function equations are coupled to yield an exact-condensed synthesized structure vibration equation in frequency domain, from which the generalized structural frequency-response functions are obtained. Substructural frequency-response functions are calculated separately by using the generalized frequency-response functions, which can be assembled into an entire-structural frequency-response function matrix. Substructural power spectral density functions are expressed by the exact-synthesized substructural frequency-response functions, and substructural random responses such as correlation functions and mean-square responses can be calculated separately. The accuracy and capacity of the proposed substructure synthesis method is verified by numerical examples.

• 한국해양공학회지
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• 제25권2호
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• pp.7-14
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• 2011

Numerical simulations were performed for the evaluation of wave and current loads on a fixed cylindrical substructure model for an ocean wind turbine using the ANSYS-CFX package. The numerical wave tank was actualized by specifying the velocity at the inlet and applying momentum loss as a wave damper at the end of the wave tank. The Volume-Of-Fluid (VOF) scheme was adopted to capture the air-water interface. An accuracy validation of the numerical wave tank with a truncated vertical circular cylinder was accomplished by comparing the CFD results with Morison's formula, experimental results, and potential flow solutions using the higher-order boundary element method (HOBEM). A parametric study was carried out by alternately varying the length and amplitude of the wave. As a meaningful engineering application, in the present study, three kinds of conditions were considered, i.e., cases with current, waves, and a combination of current and progressive waves, passing through a cylindrical substructure model. It was found that the CFD results showed reasonable agreement with the results of the HOBEM and Morison's formula when only progressive waves were considered. However, when a current was included, CFD gave a smaller load than Morison's formula.

• 대한토목학회논문집
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• 제33권2호
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• pp.443-453
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• 2013

하이브리드 실험은 수치해석 모형과 물리적 부분구조 모형사이의 상호작용을 통하여 구조물의 거동을 예측하는 실험법이다. 본 연구에서는 지진하중 재하 시 1경간 2층 강 뼈대 구조물에 대한 다자유도 하이브리드 실험을 수행하고 유효성을 확보하는데 그 목적이 있다. 이를 위해 전용 하이브리드 수치해석 프로그램인 FEAPH을 개발하였으며, 최적화된 시스템을 구축하였다. FEAPH은 고정 반복법(Fixed iteration)과 병렬화(Parallelization) 기법을 적용하여 순차적 해석에서 발생되는 비효율적 연산을 개선하였다. 또한, 종전에 데이터 통신과 부분구조물과 해석프로그램간의 인터페이스를 간략화하여 하이브리드 시스템 구성을 최적화 하였다. 그 결과, 입력 가진시간(30초) 대비 약 10%의 실험시간이 소요되었다. 시스템의 신뢰성을 검증하고 선형실험과 강 뼈대 구조물의 동적거동을 예측하기 위해 비선형 실험을 수행하였으며 수치해석과의 변위응답이력은 거의 일치 하였다. 그러나 최대변위에 대한 응답은 다소 차이를 보였으며, 이는 재료 비선형성에 대한 해석상의 오차와 영구변형에 의해 발생한 것으로 판단된다. 따라서 적절한 재료 비선형 모델과 알고리즘의 개선이 이루어지면, 실시간 하이브리드 시스템은 구조물의 동적거동을 예측하는데 유용하게 활용될 것이며, 추후 진동대 실험을 대체할 수 있는 효과적인 실험 방법이 될 것으로 판단된다.