• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2000년도 춘계 학술대회논문집
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• pp.127-139
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• 2000

Transient aerodynamic response of an airfoil to a rapidly deploying spoiler is numerically investigated using a two-dimensional turbulent compressible Navier-Stokes flow model. The spoiler moving relative to a stationary airfoil is treated by an overset grid bounded by a 'dynamic domain-dividing line' the concept of which is developed first..in this paper. The fluid-dynamic mechanism of the adverse lift due to the rapidly deploying spoiler is analyzed. Also the effect of spoiler deploying rate on the initial behavior of the aerodynamic response is expounded, which is of interest in view of active control technology and controller design for the spoiler. The results of present computation about the stationary as well as moving spoilers are relatively in good agreement with the existing experimental data.

• 대한방사선치료학회지
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• 제7권1호
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• pp.176-184
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• 1995

It is very useful benefits to use the megavoltage photon beams in deep site tumor radiotherapy for skin sparing effects. But, In some cases of head and mock tumors, it is often necessary to use spoiler for rapid buildup on skin region. A spoiler with tissue equivalent material to be moved between the patients and the collimator can increase or control the skin dose and buildup region due to position and thickness of the spoiler was measured. Then, the effect of spoiler on skin dose and build up region in protruded tumor of head and neck was evaluated quantitatively. The measurements were abtained with PTW 2334 chamber (Markus type) on a polystylene phantom for 6MV x-ray from an accelerator.

• 한국항공우주학회지
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• 제48권5호
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• pp.335-342
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• 2020

스텔스 성능을 향상시키기 위해 꼬리날개를 제거한 무미익 항공기는 러더(rudder)를 대체하여 스포일러(spoiler)를 활용하여 방향조종을 수행한다. 짧은 시간에 스포일러 작동을 반복하는 경우 비정상적(unsteady)이고 비선형적인 공력특성이 발생하여 항공기 비행성능에 역효과(adverse effect)를 초래할 수 있다. 본 연구에서는 dynamic mesh 기법을 적용한 전산해석을 통하여 스포일러 전개에 따른 에어포일의 비정상 공력 특성을 해석하였다. 스포일러 전개 속도, 장착 위치, 전개 스케줄(deployment scheduling) 변화에 따른 공력특성을 분석하여 스포일러의 동적 작동에 따른 역효과를 감소시킬 수 있는 방안을 검토하였다. 스포일러 장착위치 및 전개 방식의 적절한 선정을 통해 스포일러 동적 역효과를 감소시킬 수 있음을 확인하였으며, 에어포일 형상최적화를 통한 역효과 감소방안에 대한 추가적인 연구가 필요한 것으로 판단된다. 이러한 동적 공력 데이터는 향후 무미익 형태의 항공기 개발에 기초자료로 활용될 수 있을 것이다.

• 한국산학기술학회논문지
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• 제19권2호
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• pp.689-694
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• 2018

최근 친환경 자동차 개발과 함께 대기 오염 문제 대응을 위해서 자동차 연비 개선은 차량 개발에 있어서 매우 중요하다. 개발 차량의 연비 향상을 위한 요소 중 차량 외관을 타고 흐르는 공기 흐름과 차량 후부에서의 공기 유동 현상은 중요한 요소이다. 특별히 SUV(Sports Utility Vehicle) 차량의 차량 후부 공기 유동은 리어 스포일러 설계 시 고려해야 하는 중요한 설계 항목 중 하나이다. 본 연구에서는 차량의 공기 유동에 영향을 주는 리어 스포일러의 제어 인자를 정하고 각 제어 인자의 공기 유동 특성에 대한 민감도를 시험을 통하여 비교 분석하고, 유동 저항력을 감소시킬 수 있는 스포일러의 최적 제어 인자를 결정하였다. 결정된 최적 제어 인자를 이용한 시험 모델을 만들어 시험평가하고 그 결과 값에 대한 S/N비와 평균값을 분석하여 제어 인자 값을 변경하였다. 변경된 최적 제어 인자 값을 이용한 개선 모델을 다시 제작하고 유동 시험을 실시하여 공기 저항력 감소 효과와 원가절감 효과를 확인하였다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2005년도 추계학술대회논문집
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• pp.196-199
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• 2005

Flow traveling over a cavity opening forms a vortex due to unstable shear layer and induces an aerodynamic pressure excitation from the diffusion of the vortex convecting out of the trailing edge of the opening. The interaction between the excitation force and the cavity response sustains resonance in the resonator(cavity) and locked-in vortex shedding at the leading edge of the opening. The aerodynamic excitation force can be described from the diffusion of the vortex over the trailing edge and the level of its diffusivity is related to the strength of vorticity seeded at the loading edge. In this study, the control scheme of the internal pressure oscillation was proposed from regulating the vorticity at the leading edge by use of an oscillating spoiler. It was found that the relative motion between the spoiler and the air mass at the cavity opening influenced vorticity strength and the control was achieved by direct feedback of the cavity pressure fluctuation to the actuator.

• 한국소음진동공학회논문집
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• 제17권12호
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• pp.1223-1229
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• 2007

Flow traveling over a cavity opening forms a vortex due to unstable shear layer and induces an aerodynamic pressure excitation from the diffusion of the vortex convecting out of the trailing edge of the opening. The interaction between the excitation force and the cavity response sustains resonance in the resonator(cavity) and locked-in vortex shedding at the leading edge of the opening. The aerodynamic excitation force can be described from the diffusion of the vortex over the trailing edge and the level of its diffusivity is related to the strength of vorticity seeded at the leading edge. In this study, the control scheme of the internal pressure oscillation was proposed from regulating the vorticity at the leading edge by use of an oscillating spoiler. It was found that the relative motion between the spoiler and the air mass at the cavity opening influenced vorticity strength and the control was achieved by direct feedback of the cavity pressure fluctuation to the actuator.

• 한국기계가공학회지
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• 제5권3호
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• pp.17-22
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• 2006

Sunroof is getting widely used in automobiles since it maintains, compare to window, better air circulation as well as less noise while driving in high speed. In this study, we consider an electronic control type spoiler sunroof which slides backward after tilting a rear part of a glass. Installing a wind deflector on the sunroof reduces noise much more effectively. The height of the wind deflector is designed using a boundary theory related to incompressible air layer. The developed wind deflector is investigated experimentally by measuring a wind noise. When the height of the wind deflector is designed by a fixed type, the sunroof maintains a very quiet interior noise over a certain driving speed, nevertheless it produces relatively loud noise in low driving speed.

• 한국항공우주학회지
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• 제47권6호
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• pp.422-428
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• 2019

수직미익이 없는 전익기 형상은 낮은 레이더반사면적(RCS) 특성으로 인해 최근 UCAV를 위한 대표적인 형상으로 대두되고 있다. 무미익 전익기 형상은 방향축 관점에서 보면 정적으로 불안정하면서도 이를 효과적으로 제어하기 위한 수직 조종면이 없다는 두 가지 난제를 모두 갖고 있다. 이같은 형상을 제어하기 위해서는 추력 벡터링을 적용하거나 날개의 항력차이를 이용하는 드래그 러더(Drag Rudder) 형태의 에일러론 또는 스포일러 등을 적용할 수 있다. 본 논문에서는 전익기 형상의 횡방향축 공력특성 및 드래그 러더 중 스포일러 형태의 조종면에 대한 공력특성을 설명한다. 또한, PI 구조의 제어설계 기법을 사용하여 전익기의 횡방향축 운동을 효과적으로 제어할 수 있음을 제시하고, 비행시험을 통하여 설계된 제어기로 안정적인 비행이 가능함을 보였다.

• Journal of Microbiology and Biotechnology
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• 제28권1호
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• pp.77-86
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• 2018

The human pathogen and food spoiler Bacillus cereus can form biofilms that act as a persistent source of contamination, which is of public health concern. This study aimed to understand how the source of isolation might affect the behavior of biofilm formation. Biofilm formation abilities of 56 strains of B. cereus isolated from different environments, including human food poisoning, farm, and food, were determined. Crystal violet assay results revealed significant (p < 0.05) differences in biofilm formation abilities among the strains isolated from different sources only at an early stage of incubation. However, strain origin showed no impact on later stage of biofilm formation. Next, correlation of the group of isolates on the basis of their biofilm-forming abilities with the number of sessile cells, sporulation, and extracellular polymeric substance (EPS) formation was determined. The number of sessile cells and spores in biofilms was greatly influenced by the groups of isolates that formed dense, moderate, and weak biofilms. The contribution of extracellular DNA and/or proteins to EPS formation was also positively correlated with biofilm formation abilities. Our results that the source of isolation had significant impact on biofilm formation might provide important information to develop strategies to control B. cereus biofilm formation.

• 한국철도학회:학술대회논문집
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• 한국철도학회 2010년도 춘계학술대회 논문집
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• pp.133-138
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• 2010

This paper describes on aerodynamic characteristics of pantograph system for Next generation high speed train(HEMU-400). The pantograph which supports electric power is located on the roof. Because of this, it generate high drag, severe acoustic noise and vibration which induced unstable flow due to complex configuration. Therefore, the design of high efficient pantograph needs to increase operational speed. In this research, wind tunnel tests were performed to design a high efficient pantograph system using 1/4 scaled model which were KTX-II pantograph, single arm pantograph and periscope type pantograph with square cylinder shape panhead and optimized shape panhead. For real operational condition, flow directions were adapted by rotation of pantograph. From this results of wind tunnel, it is checked that the pantograph with optimized panhead and single arm type or periscope type has better aerodynamic performance. In addition, lift control device and spoiler in pantograph were tested to investigate the validity of application.