• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2007.11a
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• pp.165-169
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• 2007

Qualification test range for Lox/Kerosene gas generator cyle liquid rocket engine was determined by considering engine dispersion and flight inlet conditions. With various pump characteristics, the operation range of components and system was investigated through dispersion analysis. The variation of engine performance shows opposite trends in calibration and dispersion.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2007.11a
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• pp.325-328
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• 2007

In this study, intended to high flight condition test, air flow test and environmental condition test of Small-sized Gas Turbine (including auxiliary power utility - APU) improve preexisting large size test stand C-9N(SCIAM) in Russia. In the process of developing C-9N test stand, this study includes conceptual design approach. This test stand consists of environmental condition, thermostat, cooling/drying, thrust measuring system and SAR (system of automatic regulation).

• Journal of the Korean Society of Propulsion Engineers
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• v.15 no.6
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• pp.91-97
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• 2011

A test range for a 75tf class gas generator cycle liquid propellant rocket engine is defined. The engine system test range is defined by the performance variation during flight, the dispersion after engine calibration, and additional margin. The component development test range includes the operation range corresponding to the engine system test range and the component performance margin.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.21 no.12
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• pp.1615-1623
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• 1997

Numerical study on the chaotic stirring of the screw extruder model proposed has been performed. The velocity field was used in obtaining the trajectories of passive particles for studying the stirring effect of the screw extruder. Two nonlinear dynamical tools, that are Poincare sections and Lyapunov exponents, were used in analysing the stirring effect. The Poincare sections and the Lyapunov exponents show that the stirring effect is most satisfactory, when n(the number of flights in a section) is 1, for the case a (aspect ratio ; flight height divided by the spacing between flights) being O.1. It is also required to set n=3, or 5 at a= 0.2, 0.3 for a uniform stirring.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.28 no.12
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• pp.1511-1520
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• 2004

A flow visualization of the two-dimensional rigid fling-clap motions of the flat-plate wing are performed to gain knowledge of butterfly mechanisms that might be employed by butterflies during flight. In this numerical visualization, the time-dependent Navier-Stokes equations are solved for cyclic fling and clap types of wing motion. The separation vortex pair that is developed in the fling phase of the cyclic fling and clap motion is observed to be stronger than those of the fling followed by clap and pause motion(1st cycle motion). This stronger separation vortex pair in the fling phase is attributable to the separation vortex pair of the outside space developed in the clap phase as it moves into the opening in the following fling phase. Accordingly, higher lift and power expenditure coefficients in the fling after clap phase is caused by the stronger separation vortex pair.

• Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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• 2001.11b
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• pp.378-381
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• 2001

The electron drift mobility of poly(4,4'-cyclohexylidenediphenyl carbonate) (PC-Z) doped with 3,5-dimethy-3,5-di-t-butylstilbenequinone(MBSQ), 3,5,3,5-tetra-t-butyl stilbenequinone(TBSQ) and 3,5,3,5-tetra-methyl stilbenequinone(TMSQ) was measured by the time-of-flight technique. The electric field and temperature dependences of the electron drift mobility were discussed with Poole-Frenkel, Arrhenius formulations and non-Arrhenius type of temperature dependence. It was assumed that the hopping sites were Gaussian distribution. Mobility and activation energy of MBSQ were increased with increasing dopant. However, mobilities and activation energy of TBSQ and TMSQ were increased and decreased, respectively.

• Transactions of the Korean Society of Machine Tool Engineers
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• v.14 no.5
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• pp.80-86
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• 2005

High velocity oxy-fuel thermally sprayed coating of the WC-Co cermet material is a well-established process for modifying the surface properties of the structural components exposed to the corrosive and wear attacks. The hard WC phase in the coating resists to the wear while the soft metallic Co increases the adhesive and cohesive bonding properties. The coating properties deposited by the HVOF process are greatly dependent on the feedstock materials and processing parameters. The effects of the feedstock material and process coating parameters including the in-flight particle parameters and resultant coating microstructures were observed in this paper.

• Proceedings of the Korean Society of Broadcast Engineers Conference
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• 2012.11a
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• pp.37-39
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• 2012

최근 ToF(Time-of-Flight) 방식의 깊이 센서 카메라가 깊이 영상 획득에 많이 사용되고 있다. 그러나 ToF 깊이 카메라가 제공하는 깊이 영상은 센서의 물리적 한계로 인해 잡음이 존재한다. 따라서 고품질의 깊이 영상을 얻기 위해서는 깊이 영상의 잡음을 제거해 주는 것이 필수적이다. 일반적으로 깊이 영상의 잡음 제거에는 joint bilateral filter 를 사용한다. Joint bilateral filter 는 기준 화소와 그 주변 화소의 색상 영상의 밝기 차이값과 화소간 거리값에 각각 가우시안 함수를 적용하여 joint histogram 을 생성하고 그 평균값을 기준 화소의 깊이값으로 채운다. 하지만 이 과정에서 깊이 영상의 경계 영역에서 흐려짐 현상이 발생한다. 경계영역에 발생한 흐려짐 현상은 최종적인 3D 입체 콘텐츠의 품질을 저하시킨다. 본 논문에서는 이와 같은 문제점을 해결하기 위해 joint histogram 의 최고점을 찾아 기준 화소의 깊이값을 채우는 기법을 제안한다. 최고점 탐색을 통해 기존 기법의 평균값을 통해 생기는 흐려짐 현상을 줄이고 깊이 영상의 경계를 보존하면서 잡음을 제거하였다. 실험을 통하여 제안하는 기법의 우수성을 확인하였다.

• Proceedings of the Korean Society of Broadcast Engineers Conference
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• 2012.07a
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• pp.398-400
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• 2012

최근 3D에 대한 관심이 집중되면서 고품질의 3D영상을 얻기 위해 고품질의 깊이 영상이 필요하고 이를 구현하기 위한 연구가 활발히 진행되고 있다. 깊이 영상을 얻기 위해서 Time-of-Flight(ToF)방식의 깊이 센서가 활용되고 있는데 이 깊이 센서는 실시간으로 깊이 정보를 획득할 수 있지만 낮은 해상도와 노이즈가 발생한다는 단점이 있다. 따라서 깊이 센서로 생성된 저해상도 깊이맵을 고해상도로 변환해야 한다. 주로 깊이 영상의 해상도를 높이기 위해서 Joint Bilateral Upsampling(JBU) 방식이 사용되고 있다. 따라서 본 논문은 JBU 방식을 보강하여 블록단위로 분산에 따른 참조 영상의 가중치를 다르게 두어 깊이 영상의 품질을 향상시키는 방법을 제안한다.

• Proceedings of the Korean Society of Broadcast Engineers Conference
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• 2012.07a
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• pp.26-28
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• 2012

본 논문에서는 깊이 영상의 해상도를 향상시키는 기법을 제안한다. 최근 TOF(time-of-flight) 방식의 깊이 센서가 깊이 영상 획득에 많이 사용되고 있다. 그러나 TOF 깊이 센서가 제공하는 깊이 영상은 대부분 저해상도이기 때문에 고해상도의 콘텐츠 제작을 위해서는 깊이 영상의 해상도를 향상시켜주는 것이 필수적이다. 본 논문에서는 깊이 영상의 해상도를 높이기 위하여 적응적 가중치 보간법을 적용한 후, Bilateral 필터링을 수행하여 품질을 높인다. 일반적으로 영상의 해상도를 높일 때 보간법을 많이 사용하는데, 본 논문에서는 이러한 보간법들을 사용하여 깊이 영상의 해상도를 높였을 때보다 제안하는 기법의 성능이 우수함을 실험을 통해 확인하였다.