• 대한조선학회논문집
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• 제44권3호
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• pp.267-278
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• 2007

This experimental study investigated on the eddy making effect on the roll motion of a rectangular barge in a two-dimensional wave tank. The structure was used to simulate a simplified rectangular barge in the beam sea condition. The structure with a draft one half of its height was hinged at the center of gravity and free to roll by waves. The rectangular barge was tested with regular waves with a range of wave periods that are shorter, equal to, and longer than its roll natural period. Particle image velocimetry (PIV) was employed to obtain the velocity field in the vicinity of the structure. The coupled interactions between the incident wave and the barge were demonstrated by examining the vortical flow fields to elucidate the eddy making effect during the roll motion. For incoming wave with a wave period same as the roll natural period, the barge roll motion was reduced by the eddy making damping effect. At the wave period shorter than the roll natural period, the structure roll motion was slightly reduced by the vertical flow around the barge. However, at the wave period longer than the roll natural period, the eddy making effect due to flow separation at structure corners indeed amplifies the roll motion. This indicates that not only can the eddy making effect damp out the roll motion, it can also increase the roll motion.

• 한국항공우주학회지
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• 제40권9호
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• pp.745-751
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• 2012

하이브리드 로켓은 축 방향의 산화제 유동과 고체 연료의 기화로 인한 벽면 분출 유동사이의 상호 간섭에 의해 복잡한 형태의 혼합 전단층이 존재한다. 연소실 입구에 링이 설치되어 있고 질량분사가 있는 실린더 유동에 대하여 압축성 효과를 고려한 LES(Large Eddy Simulation) 기법을 적용하여 수치계산을 수행하였다. 최근의 실험에 의하면 연료 중간에 링과 같은 다이아프램이 설치된 경우, 연소율의 증가가 관찰되었다. 계산 결과에 따르면, 축방향 유동과 벽면 분출 유동이 상호 간섭하여 발생하는 벽면 와류가 국부적인 연료 표면으로의 열전달을 증가시켜 실험에서 관찰되는 딤플이 생성되는 것을 확인하였다. 또한 연소실 입구에 설치된 링에 의하여 발생되는 와류는 벽면 와류가 보다 활발하게 생성되고 열전달과 혼합을 향상시키는 역할을 하며 이 때문에 연소율이 증가되는 것으로 보인다.

• Advances in aircraft and spacecraft science
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• 제4권4호
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• pp.353-369
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• 2017

Flutter is a dangerous phenomenon encountered in flexible structures subjected to aerodynamic forces. This includes aircraft, buildings and bridges. Flutter occurs as a result of interactions between aerodynamic, stiffness, and inertia forces on a structure. In an aircraft, as the speed of the flow increases, there may be a point at which the structural damping is insufficient to damp out the motion which is increasing due to aerodynamic energy being added to the structure. This vibration can cause structural failure, and therefore considering flutter characteristics is an essential part of designing an aircraft. Scientists and engineers studied flutter and developed theories and mathematical tools to analyze the phenomenon. Strip theory aerodynamics, beam structural models, unsteady lifting surface methods (e.g., Doublet-Lattice) and finite element models expanded analysis capabilities. Periodic Structures have been in the focus of research for their useful characteristics and ability to attenuate vibration in frequency bands called "stop-bands". A periodic structure consists of cells which differ in material or geometry. As vibration waves travel along the structure and face the cell boundaries, some waves pass and some are reflected back, which may cause destructive interference with the succeeding waves. This may reduce the vibration level of the structure, and hence improve its dynamic performance. In this paper, for the first time, we analyze the flutter characteristics of a wing with a periodic change in its sandwich construction. The new technique preserves the external geometry of the wing structure and depends on changing the material of the sandwich core. The periodic analysis and the vibration response characteristics of the model are investigated using a finite element model for the wing. Previous studies investigating the dynamic bending response of a periodic sandwich beam in the absence of flow have shown promising results.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2006년도 추계학술대회논문집
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• pp.65-68
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• 2006

Experiments were performed to investigate the effects of mud-flap width on the aeroacoustic noise generation inside high-speed trains. The open-circuit type wind tunnel was used. The measurement setup was custom-built to simulate intercoach spacing. From the measurements, the characteristics of the turbulent flow after the intercoach spacing and consequent generation of aeroacoustic noise inside the cabin was investigated. Especially the effects of mud flap length on the characteristics of the characteristics of the turbulent flow were identified. The mechanism of noise generation by analyzed interactions with structure vibration characteristics and generation characteristics of blocked pressure was investigated.

• 한국산업융합학회 논문집
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• 제21권5호
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• pp.191-195
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• 2018

By using an ANSYS product suite (CFX, Ansys Multiphysics), which is a powerful tool for multiphysics analysis of complicated physical phenomena, we performed a structural stress analysis based on fluid flow and heat transfer phenomena within a quick connect/disconnect (QC/DC) bellows system. Considering the extremely low temperatures in the QC/DC environment, an approach to the problem based on complex multi-physics phenomena, where different phenomena interact with each other, is crucial. Therefore, we use a numerical analysis technique where fluid-thermal-structural interactions are combined. In conclusion, when low temperature fluids flow inside bellows, the expected service life is conspicuously reduced due to the thermal stress caused by heat transfer. Therefore, in future research, a structure with considerably reduced thermal stress by robust design optimization will be derived.

• Advances in nano research
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• 제13권4호
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• pp.341-350
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• 2022

The continuous elements method, also known as the dynamic stiffness method, is effective for solving structural dynamics problems, especially over a large frequency range. Before applying this method to fluid-structure interactions, it is advisable to check its validity for pure acoustics, without considering the different coupling parameters. This paper describes a procedure for taking wave propagation into account in the formulation of a Dynamic Stiffness Matrix. The procedure is presented in the context of the harmonic response of acoustic pressure. This development was validated by comparing the harmonic response calculations performed using the continuous element model with the analytical solution. In addition, this paper illustrates the application of this method to a simple compressible flow problem, since it has been applied solely to structural problems to date.

• 대한지리학회지
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• 제47권2호
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• pp.268-281
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• 2012

인구이동통계는 사회현상에 대한 공간적 이해와 공간과정의 사회적 영향 파악에 유용한 정보를 제공해줌에도 불구하고 데이터 구조의 복잡성 때문에 자료 서비스와 분석이 제한되어 왔다. 한편 인구이동통계를 탐색하고 시각화하는 효과적인 방법인 유선도 작성(flow mapping)은 아직 상용 GIS 소프트웨어서 완전히 구현되지 못하고 있다. 이에 본 연구의 목적은 Web GIS를 통한 유선도 제작과 이를 이용한 인구이동통계에 대한 탐색적 공간 분석이 가능함으로 보여주는 것이다. 데이터베이스, GIS, 지도학적 관점에서 인구이동통계의 특성을 고찰하였고, 이를 바탕으로 O-D 구조의 인구이동통계를 유선도 제작에 적합한 공간데이터로 변환하였다. 인구이동통계에 적합하도록 Web GIS의 사용자 인터페이스를 전문화하였고, 지도화의 시간, 공간 및 속성 범위의 설정을 통한 탐색적 시각화가 가능하도록 구성하였다.

• 한국해양공학회:학술대회논문집
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• 한국해양공학회 2006년 창립20주년기념 정기학술대회 및 국제워크샵
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• pp.403-406
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• 2006

A particle method recognized as one of gridless methods has been developed to investigate the nonlinear free-surface motions interacting to the structures. The method is more feasible and effective than convectional grid methods in order to solve the flow field with complicated boundary shapes. In the present study, breaking waves with a floating body are simulated to investigate fluid-structure interactions in the coastal zone.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 추계학술대회
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• pp.508-513
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• 2003

Experiments are performed to investigate the detailed structure of underexpanded twin jet impinging on a perpendicular flat plate. The major parameters, such as nozzle operating pressure and nozzle spacing, are varied to create different jet flow fields resulted from the complicated interactions of the twin jets. From the surface pressure measurements and shadowgraphs taken by schlieren optical system, the jet structure is strongly dependent on the nozzle operation pressure and the spacing. The results obtained show that the closer nozzle spacing may induce to decrease the diameter of the Mach disk within the first shock cell in the underexpanded twin jet. With the increasing nozzle operating pressure and decreasing the nozzle spacing, a new shock wave appears at the entrainment region between the two jets, due to the enhancement of mixing effect of the both jets. The closer nozzle spacing makes the overall impinging pressure level higher, while severe pressure oscillation along the axis of symmetry. Furthermore it is recommended the wider spacing to obtain higher thrust under the present experimental conditions.

• 대한화학회지
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• 제58권6호
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• pp.560-568
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• 2014

단백질 폴딩 반응에서 정전기적 상호작용의 역할을 라이신 29를 알라닌으로 치환한 변이 유비퀴틴을 사용하여 탐색하였다. 유비퀴틴의 입체구조에서 라이신 29의 곁사슬은 글루탐산 16과 아스파르산 21의 곁사슬과 근접한 거리에 있어서 곁사슬끼리 정전기적 상호작용을 통하여서 삼차원 입체구조를 안정화시킬 것으로 예측되었다. 라이신을 알라닌으로 치환하여 정전기적 상호작용을 제거하였을 때 유비퀴틴의 native state의 구조적 안정성이 ~20% 감소한 점은 라이신 29에 의한 정전기적 상호작용이 단백질 삼차구조의 안정성에 상당히 기여하고 있다는 점을 시사하였다. 폴딩 반응의 진행 과정을 stopped-flow 장치로 측정한 folding kinetics 실험은 이전에 관찰된 것과 마찬가지로 unfolded state에서 native state로 진행하는 과정에 중간단계를 거치는 three-state on-pathway 메커니즘을 따르는 것으로 나타났다. 더욱이 라이신 29에 의한 정전기적 상호작용이 중간단계의 구조적 안정성에 기여하는 정도가 native state의 구조적 안정성에 기여하는 정도의 ~55%인 것으로 나타났다. 이는 유비퀴틴 폴딩의 중간단계의 구조도 라이신 29에 의한 정전기적 상호작용에 의하여 상당히 안정화 된다는 것을 의미하며 따라서 정전기적 상호작용이 단백질 삼차원 입체구조의 골격이 완성된 폴딩의 마지막 단계에 형성되어 단백질 native state의 안정성에만 기여하는 것이 아니라 중간단계가 형성되는 폴딩 반응의 초기에도 형성되어 폴딩 반응을 이끌어가는데도 기여한다는 것을 의미한다.