• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.04a
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• pp.433-436
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• 2011

The effect of plasma on flow characteristics in subsonic flow in backward-facing step is studied. The velocty of main flows are 0.5 m/s. DBD plasma is using for flow control. Stainless foil and polymide films are used as an electrode and dielectric material. The change of flow characteristics are shown by different of plasma generation region in fluid flow.

• Proceedings of the KSME Conference
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• 2005.11a
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• pp.73.1-73.1
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• 2005

• Journal of the Korean Society of Propulsion Engineers
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• v.19 no.6
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• pp.33-41
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• 2015

Scaled model of a dual-mode ramjet engine with large backward-facing step, as a component of the rocket-based combined cycle engine, was designed. Design parameters were derived for this engine with the consideration of application for the rocket-based combined cycle engine. Design methodology was established for these design parameters. The design was partially verified through numerical study. Flow characteristics of the dual-mode ramjet engine with large backward-facing step was investigated experimentally. The design methodology for relevant design parameters established in this study was verified as feasible.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.14 no.7
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• pp.692-698
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• 2003

This paper presents IM model which is produced in 3 port RF passive component. We calculated forward and reflect PIM of 3 port component by using the model. And they are reasonable agreement with measurement result like below. In the case of forward IM, calculated result is -122 dBc(at 43 dBm), which differ 2.5 dB with measurement result. And reflected IM, the average calculated result is -130 dBc(at 43 dBm), which differ 3 dB with measurement result. The results which are calculated and measured under various condition(IM source level, frequency sweep, contour length, etc.) show that forward method gets more fixed result than that of reflect. Consequently, PIM of 3 port component is predicted and analyzed for desensitizing by the proposed model.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.40 no.10
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• pp.833-839
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• 2012

In this paper, we analyze the reconstruction error in the modeling of flow field on BFS(Backward Facing Step). In order for the mathematical modelling of a density on the field, the spatial and temporal modes are extracted by POD(Proper Orthogonal Decomposition) method. After formulating the modeling error, we summarize the relationship between the energy strength and the reconstruction errors. Moreover the allowable modeling error limits in the flow control point of view are confined by analysing in the frequency domain as well as time domain of the reconstructed data.

• Proceedings of the Korea Society for Industrial Systems Conference
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• 1997.03a
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• pp.183-193
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• 1997

추론엔진과 지식베이스를 기반으로 하는 전문가 시스템은 사용목적에 맞게 구성되며,인간의 사고 방식을 모방한 컴퓨터가 올바른 해를 도출시키도록 하는데 궁극적인 목표가 있다. 즉, 추론의 효율성이 전문가 시스템의 효율성을 좌우한다. 시스템이 어떠한 목적을 갖는가에 따라서, 추론 방법과 지식표현 방법등이 결정된다. 최근 추론의 효율성을 극대화하기 위해 이용되고 있는 지식표현 및 추론 방법으로는 Rete, TREAT 등의 트리 표현을 사용하는 전향추론, 관계리스트를 사용하는 직접추론 등이 있다. 전문가 시스템의 성능은 추론을 얼마나 효율적이고 정확하게 하는지에 따라 좌우된다. 본 논문에서는 이러한 추론의 효율성이 지식베이스의 구축형태와 밀접한 관련을 이용하여 효율적인 추론 엔진을 구성하였다. 지식의 표준화가 모듈화가 쉬운 생성규칙을 사용하여 지식을 표현하였으며 , 사용자의 요구에 의해 전향추론, 후향추론이 수행되도록 하였다. 본 논문에서는 추론을 효율적으로 하기위한 기본 방법중, 지식표현을 보다 더 효과적으로 구축하는 방법을 택하였다. 기존의 지식표현방법을 살펴보고, 이를 기반으로 새로운 지시표현 방법인 ECBM(extedned clause bit matrix)과 ERCBM(extended clause bit matrix)을 제안하고 이를 이용하여 전향추론, 후향추혼이 가능한 추론엔진을 구축하였으며 이 두 지식표현을 이용하여 구축되어진 추론엔진을 비교하였다. 이 추론엔진은 기존에 시스템과는 달리 전향, 후향이 모두 효율적으로 수행되어지며, 모든 지식에 대해 적용이 가능한 강력한 범용성을 갖고 있다.

• Journal of Korean Philosophical Society
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• v.105
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• pp.269-290
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• 2008

The purpose of this paper is to explore the possibility of backwards causation. For study, this paper was divided into four views as follows: The first view was sometimes suggested by the people such as M. Dummett who distinguished observers from behaviors. According to observers' view, backwards causation is impossible, whereas behaviors' view possible. However, in a real or genuine sense, it is incorrect for us to argue for impossibility of backwards causation from the observer aspect. The second view was supported by J. H. Schmidt. He analyzed the possibility of backwards causation in terms of macro and micro level analysis about the causal events. According to micro level analysis, backwards causation is possible, but macro level analysis impossible. Usually the latter makes the former something miraculous. Under the macro level analysis, backwards causation, at first, seems to be miraculous phenomena which belongs to the micro level analysis. The third view had to do with physical equation, and the fourth view physical phenomena, respectively. John Earman argued for the backwards causation by the transformation from Lorentz­-Dirac equation to a second-order integro-differential one in the field of electrodynamic acceleration. His argument was criticized because of his misunderstanding about the relationship between two equations. On the other hand, Phil Dowe defended a version of Reichenbach's own theory about the direction of causation founded on the fork asymmetrical causal relation. However his view was different from Reichenbach's because the former defended the backwards causation model of Bell phenomena in quantum mechanics. On the contrary, Reichenbach put stressed on the priority of cause in the causal process. Subjectivism has recently been defended by H. Price, under the label of perspectivism. According to him, in a certain sense causal asymmetry is not in the world, but is rather a product of our own asymmetric perspective on the world. He also suggested causal net, the symmetry of microphysics, and so on. As mentioned above, there are many kind of suggestions of backwards causation. However none of them replaced objectively the main streams of the direction of causal process. The main stream has been usually defended by pragmatical ground. That is, effects do not precede their causes although causes cannot be without their effects.

• 한국전산유체공학회:학술대회논문집
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• 2010.05a
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• pp.40-42
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• 2010

Unsteady CFD results of the backward facing step (BFS) flow field is reconstructed by the low-dimenstional modes using the POD (Proper Orthogonal Decomposition) technique. Flow responses to the blowing or suction with various frequencies and amplitudes applied at the edge of the BFS can also be analysed using the same technique. The present technique can be effectively applied to the feedback flow control device.

• 월간산업보건
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• s.46
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• pp.16-20
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• 1992

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.1
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• pp.97-103
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• 2003

Numerical research has been done for the transverse jet behind a rearward-facings step in turbulent supersonic flow without chemical reaction. Purpose of transverse jet is to enhance mixing of the fuel in the combustor. Two-dimensional unsteady flowfields generated by slot injection into supersonic flow are numerically simulated with the Navier-Stokes equations with two-equation k-$\varepsilon$ turbulence model. Numerical method is used high-order upwind TVD scheme. Eight cases are computed for different slot momentum flux ratios and slot position at downstream of the step. The flow is very similar to the cavity flow, because the jet acts as an obstacle. The numerical results thus show the periodic phenomenon.