• 천문학회보
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• 제35권2호
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• pp.48.2-48.2
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• 2010

Quiescent filaments are bigger, more stable, and longer lived than active region filaments. So, the shape of a quiescent filament changes little during its lifetime and a fast motion of plasma rarely occurs. But when it is dynamically influenced by external phenomena, a rapid motion of plasma may temporarily occur. By analyzing the motion of plasma we can infer some of the magnetic structure permeating such an excited quiescent filament. We analyzed the H$\alpha$ images of a quiescent filament in the northern hemisphere that was observed at Big Bear Solar Observatory on 2004 August 2, and found that: 1) the filament was excited by a flare that occurred in a remote active region located in the southern hemisphere, 2) By this excitation, a part of the filament moved vertically upward and horizontally out of main body, and then it stayed there without much motion. Then after it moved vertically downward and horizontally to the main body, 3) the final position of plasma, however, was not the same as the initial position, being about 14Mm above it. We suggest that the filament was initially in a more or less static equilibrium. The excitation of the filament broke the initial equilibrium, and then brought about a new one that is different from the original one. Since the filament should have magnetic field, it is likely that both the equilibria may have been maintained by diplike magnetic structures. Furthermore, the transition from one equilibrium to another as we inferred should have accompanied a permanent change of magnetic configuration as well.

• 대한전자공학회논문지SP
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• 제38권2호
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• pp.149-159
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• 2001

기존의 블록기반 움직임 예측방법은 특히 저전송률 비디오 압축에 사용 될 경우 움직임 필드에서의 블록화 현상이나 불안정한 움직임 예측과 같은 문제를 수반한다. 본 논문은 이러한 단점을 극복하기 위해 H.263의 기존 블록기반 DCT부호화 구조를 최대한 유지하면서 비정형 삼각형 메쉬에 기반한 새로운 움직임 보상 방법을 수용할 수 있는 하나의 방법을 제안한다. 제안방법은 복원된 이전 프레임 영상을 최소의 제어점들을 이용해 표현하기 위해, 주어진 영상의 컨텐트에 적응적으로 삼각형 비정형 메쉬를 설정한다. 그리고 Affine변환에 기반한 매칭을 이용해, 설정된 각 제어점의 움직임벡터를 구한 후, 이를 이용해 각 메쉬를 Affine변환하여 예측된 현재 프레임을 얻는 전방향 움직임 보상을 제안한다. 이 방법은 컨텐트에 적응적으로 설정된 메쉬 정보를 보내지 않아도 되는 장점이 있다. 실제 비디오 데이터를 이용해 실험한 결과 제안방법이 객관적 및 주관적 화질 평가에서 기존의 블록기반 H.263 방법보다 개선되었음을 알 수 있다.

• 한국산업융합학회 논문집
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• 제2권1호
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• pp.3-15
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• 1999

It is necessary to observe the in-cylinder phenomena directly for understanding in-cylinder air motion, combustion and evaluation of the numerical simulation. This paper describes the usage, structure and peculiar technique in design, and introduces the examples of the analyses using the engine from the Honda R&D Technical Review.

• Structural Engineering and Mechanics
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• 제10권1호
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• pp.17-26
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• 2000

This paper presents a case study with a multi-degree-of-freedom (MDOF) system where the Floor Response Spectra (FRS) have been derived from a large ensemble of ground motion accelerograms. The FRS are evaluated by the frequency response function which is calculated numerically. The advantage of this scheme over a repetitive time-history analysis of the entire structure for each accelerogram of the set has been highlighted. The present procedure permits generation of FRS with a specified probability of exceedence.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 1996년도 추계학술대회 논문집
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• pp.662-667
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• 1996

For compensating the error motion of hydrostatic guideways, the structure and the theoretical design method of ACC(Active Controlled Capillary) are proposed. The maximum controllable range, micro step response and dynamic characteristics of ACC are analyzed experimentally for verifing the availability. The experimental results showed that by the use of ACC, the error motion within 2.7${\mu}{\textrm}{m}$ of a hydrostatic guideway can be compensated with the resolution of 27nm, 1/100 of uncontolled error, and the frequency band of 5.5Hz. From these results, it Is confirmed that the ACC is very effect to improve the moving accuracy of high or ultra precision hydrostatic guideways.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 2007년도 정기 학술대회 논문집
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• pp.619-624
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• 2007

Spectral element method (SEM) is introduced for the fully coupled structural dynamic problems, In this paper, the beam with passive constrained layered damping (PCLD) treatments is considered as a representative problems. The beam consists of a viscoelastic layer that is sandwiched between the base beam structure and an elastic layer, The fully coupled equations of motion for a PCLD beam are derived, The equations of motion are derived first by using Hamilton's principle, From this equations of motion, the spectral element is formulated for the vibration analysis by use of the SEM, As an illustrative example, a cantilevered beam is considered. It is shown that, as the thickness of VEM layer vanishes, the results become a simple layer beam's that.

• Earthquakes and Structures
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• 제13권1호
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• pp.9-15
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• 2017

In this paper, the influence of the rotational component, about a vertical axis, of earthquake ground motion on the response of building structures subjected to seismic action is considered. The torsional component of ground motion is generated from the records of translational components. Torsional component of ground motion is then, together with translational components, applied in numerical linear dynamic analysis of different reinforced concrete framed structure of three stories buildings. In total, more than 40 numerical models were created and analyzed. The obtained results show clearly the dependence of the effects of the torsional seismic component on structural system and soil properties. Thus, the current approach in seismic codes of accounting for the effects of accidental torsion due to the torsional ground motion, by shifting the center of mass, should be reevaluated.

• Advances in concrete construction
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• 제15권4호
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• pp.287-301
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• 2023

Hockey games attracts many fans around the world. This game requires a specific type of ball and a stick for controlling the motion and trace of the ball. This control of motion involves hitting the ball which is a direct intensive dynamic loading. The impact load transferred directly to the hand of the player and in the professional player may cause long term medical problems. Therefore, dynamic motion of the stick should be understood. In the current study, we analyze the dynamic motion of a hockey stick under impact loading from a hockey ball. In doing so, the stick geometry is simplified as a beam structure and quasi-2D relations of displacement is applied along with classical linear elasticity theory for isotropic materials. The governing equations and natural boundary condition are extracted using Hamilton's principle. The final equations in terms of displacement components are solved using Galerkin's numerical method. The results are presented using indentation and contact force values for variations of different parameters.

• 대한조선학회논문집
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• 제35권2호
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• pp.20-28
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• 1998

몰수체의 운동을 정확하게 예측하기 위해서는 동적 모형의 비선형 구조를 선택하고, 이에 해당하는 조종계수를 모형 시험을 통해 추정하여야 한다. 모형 구조가 주어지면 조종계수들의 값만이 미지수가 되어 추정은 표준 최소 자승 문제로 정식화될 수 있다. 불행하게도 몰수체들의 비선형모형 구조는 거의 알려지지 않고 있다. 따라서, 모형 시험에서 측정된 자료들로부터 운동 방정식의 구조를 결정하는 방법을 개발하여 계수 추정 절차에 중요한 한 부분으로 포함시켜야 한다. 본 연구에서는 모형 시험 결과 해석을 위해 널리 사용되고 있는 최소 자승 알고리즘과 그 성능평가법에 대해 살펴보고, Gram-Schmidt에 의한 직교 분리법에 기초를 둔 계수 식별 알고리즘을 매우 단순하고 효과적으로 구조 선택법과 계수 추정법을 결합할 수 있도록 확장하였다. 마지막으로 시뮬레이션과 실제 몰수체에 대한 모형 시험 자료로의 적용을 통해 이 기법의 성능을 검증하였다. 결론적으로 본 연구의 방법은 모형 시험 결과로부터 효율적으로 운동 방정식의 구조를 식별하고 조종 계수를 추정함을 확인하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2002년도 제18회 학술발표대회 논문초록집
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• pp.10-13
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• 2002

Pogo is the instability resulting from the interaction between rocket structure and propulsion system of liquid propellant rocket. The coupling of structure and propulsion system can lead to severe problem in rocket. For the analysis of pogo, a time-invariant linearized mathematical model is developed for a selected flight time. Propulsion system is modeled using element representations for each components. The constitutive equation of propulsion system is a homogeneous second-order equation form in the Laplace domain. Rocket structure is modeled using FEM. From the results of modal analysis of structure, the behavior of structure can be represented. System equations for coupling structure and propulsion system are composed of all propulsion system equations and vehicle motion equations reacting on the vehicle by each component of propulsion system. The stability is obtained by the eigen solution of system matrix. The optimization of the design variables such as size, place of accumulator for suppressing pogo instability is carried out. This article of study can be used to determine the degree of stability, and guide the design of pogo suppression system.