• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.34 no.6
• /
• pp.75-82
• /
• 2006

Tiltrotor aircraft can fly about twice faster and several times further than conventional helicopters. These aircraft provide advantages preventing compressibility of advancing side and stall of retreating side of blades because they take forward flight with tilting rotor systems. However, they have limit on forward flight speed because of the aeroelastic instability known as whirl flutter. First, the parametric study on the aeroelastic stability of the isolated rotor system has been performed in this paper. And the effects of pitch-link stiffness, gimbal spring constant, and precone angle on the whirl flutter stability of Smart-UAV have been investigated through CAMRAD II analysis.

• Journal of the Korea institute for structural maintenance and inspection
• /
• v.12 no.5
• /
• pp.143-151
• /
• 2008

In this paper, the optimum design of plane steel frames using second-order inelastic analysis and section increment method is presented. Since the second-order inelastic analysis accounts for geometric and material nonlinearities of the whole system as well as its component members, the design method based on second-order inelastic analysis does not require separate member capacity checks after analysis. A section increment method proposed by this paper is used as optimization technique. The weight of structures is treated as the objective function. The constraint functions are defined by load-carrying capacities, deflections, inter-story drifts, and ductility requirement. The effectiveness of the proposed method are verified by comparing the results of the proposed method with those of other method.

• Computational Structural Engineering
• /
• v.6 no.1
• /
• pp.11-16
• /
• 1993

진동기초의 해석 및 설계에서의 주요사항은 진동하중자체의 특성을 산정하는 것과 기초구조의 수평, 수직, Rocking, Pitching 응답의 해석 및 수평-Rocking이 연계된 운동의 해석이다. 현재 사용되는 진동기초설계의 해석방법은 Reissner(1936)의 반무하지반영역 위에 놓인 원형강판에 대한 해석적 결과를 이용한 여러가지 변형된 방법이 사용되고 있다. 이러한 진동기초의 해석방법은 지반의 모형화하는 방법에 따라 탄성 반무한영역으로 지반을 모형화하는 경우 (Reissner(1936), Shekhter(1948), Sung(1953), Quinlan(1953), 등)와 감쇠-탄성스프링에 의해 지반을 모형화하는 경우 (Lysmer and Richart(1966), Barkan(1962), 등)로 나눌 수 있다. 최근의 실제 설계에는 선형스프링 이론을 바탕으로 하여, 감쇠효과와 진동에 참여하는 흙의 질량영향을 무시하는 Barakan(1962)의 방법이 많이 사용되고 있다.

• Journal of the korean Society of Automotive Engineers
• /
• v.13 no.1
• /
• pp.46-56
• /
• 1991

자동차가 고르지 않은 도로를 주행할시 차체의 각 부분에 일어나는 진동을 고려하기 위해서는 차체 각 부분의 탄성효과를 고려하여야 만족할 만한 결과를 얻을 수 있다. 이 논문에서는 범용 유한요소해석 프로그램과 범용 기구해석 프로그램을 이용하여 자동차의 주행시 일어나는 차체 내의 진동에 대하여 연구하였다. 예제로는 승용차를 이용하였고 차체의 유한요소해석을 한후 그 결과를 범용 기구해석 프로그램에 이용하여 기구해석에 가장 많이 쓰이는 강체 모델의 결과와 탄성을 고려한 모델의 결과를 비교하였다.

• Journal of the Computational Structural Engineering Institute of Korea
• /
• v.20 no.5
• /
• pp.581-592
• /
• 2007

This paper deals with the elastica of deflected cantilever column with the constant volume. The columns are subjected to combined loads consisted of an axial compressive load and a couple moment at the free end. Differential equations governing the elastica of such column are derived, in which both the effects of taper type and shear deformation are included. Three kinds of taper types are considered: linear, parabolic and sinusoidal tapers. Differential equations are solved numerically to obtain the elastica of objective columns. The effects of various system parameters on the elastica are investigated extensively. Experimental studies were carried out in order to verify the theoretical results of non-linear behavior of the elasticas.

• Computational Structural Engineering
• /
• v.8 no.4
• /
• pp.65-74
• /
• 1995

Direct method developed for the inelastic analysis of planar frames subjected to monotonic loads is extended to cyclic loads. Two frame elements for Direct Method(inelastic truss and inelastic beam) are developed. The accuracy and reliability of the preposed method is verified by comparing the analysis results of example with step-by-step analysis. Direct Method is superior to Step-by-step analysis in view of reliability of solution and analysis cost.

• Journal of the Korean Society for Precision Engineering
• /
• v.24 no.3 s.192
• /
• pp.31-39
• /
• 2007

• Composites Research
• /
• v.17 no.3
• /
• pp.29-37
• /
• 2004

The aeroelastic stability analysis of composite bearingless rotors is investigated using a large deflection beam theory in hover. The bearingless rotor configuration consists of a single flexbeam with a wrap-around type torque tube and the pitch links located at the leading edge and trailing edge of the torque tube. The outboard main blade, flexbeam and torque tube are all assumed to be an elastic beam undergoing flap bending, lead-lag bending, elastic twist and axial deflections, which are discretized into beam finite elements. For the analysis of composite bearingless rotors, flexbeam is assumed to be a rectangular section made of laminate. Two-dimensional quasi-steady strip theory is used for aerodynamic computation. The finite element equations of motion for beams are obtained from Hamilton's principle. The p-k method is used to determine aeroelastic stability boundary. Numerical results are presented for selected bearingless rotor configurations based on the lay-up of laminae in the flexbeam and pitch links location. A systematic study is made to identify the importance of the stiffness coupling terms on aeroelastic stability for various fiber orientation and for different configuration.

• Journal of the Earthquake Engineering Society of Korea
• /
• v.8 no.1
• /
• pp.39-58
• /
• 2004

It is very important that predict the inelastic seismic behavior exactly for seismic performance evaluation of a building in the performance based seismic design. Evaluation method of seismic performance based on the pushover analysis reflected in PBSE was developed by some researchers. For the evaluation of inelastic global and local seismic responses by pushover analysis exactly. lateral load distribution should be adjusted and reflected the dynamic characteristics of structural system and various seismic ground motions. And performance point should be determined based on the evaluation of reasonable deformation capacity of a building more exactly. An effective method based on the improved the adaptive lateral load distribution and the equivalent responses of a multistory building is proposed in this study to efficiently estimate the accurate inelastic seismic responses. The proposed method can be used to evaluate the seismic performance for the global inelastic behavior of a building and to accurately estimate its local inelastic seismic responses. In order to demonstrate the accuracy and validity of this method, inelastic seismic responses estimated by the proposed method are compared with those obtained from other analytical methods.

• Proceedings of the Computational Structural Engineering Institute Conference
• /
• 2010.04a
• /
• pp.574-577
• /
• 2010

이번 연구에서는 저속 비압축성 유체-구조 연성을 고려한 위상 최적화을 위해 새로운 모노리틱 해석을 개발한다. 이 새로운 해석 기법에서는 기존의 유체-구조 연성 시스템 해석 기법에서 유체와 구조 영역을 분리하고 연성 조건을 만족시키는 것과 다르게 하나의 일치된 해석 방정식을 유체 영역과 구조 영역에 동일하게 적용한다. 또한, 경계조건을 만족시키기 위하여 단일화 된 해석 방정식의 물성치를 바꾸어주는 새로운 방식을 제시하였다. 이 새로운 방법에서는 유체, 구조 영역을 분리하지 않고 Navier-Stoke's 방정식과 선형 탄성식을 동시에 사용하였다. 또한, 유체-구조 영역이 연성 해석 중 변화하는 것을 반영하기 위하여 구조 변위를 이용하여 Deformation tensor를 계산하였고 이를 이용하여 변형 후에서의 Navier-Stoke 방정식의 미분을 계산하는 방법을 제안하였다. 그리고, 정상 상태 유체를 가정하고 속도에 비례하는 마찰힘인 Darcy's force 항을 Navier-Stoke 방정식에 넣고 이 마찰 힘의 크기를 변화시킴으로 해서 유체 방정식에서의 연성 경계 조건을 만족시켰다. 선형 탄성 방정식에서 Divergence이론을 이용해서 경계에서 작용하는 외력이 하는 일을 내부 시스템에 하는 일로 계산하였다. 개발된 모노리스 해석 방법을 이용하여 저속 비압축성 유체가 구조에 미치는 압축력을 계산하였고 이용하여 컴플라이언트 미케니즘을 설계하였다.