• Proceedings of the KSME Conference
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• 대한기계학회 2001년도 추계학술대회논문집B
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• pp.475-480
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• 2001

The flowfield of transverse jet in a supersonic air stream subjected to shock wave turbulent boundary layer interactions is simulated numerically by Generalized Taylor Galerkin(GTG) finite element methods. Effects of turbulence are taken into account with a two-equation $(k-\varepsilon)$ model with a compressibility correction. Injection pressures and slot widths are varied in the present study. Pressure, separation extents, and penetration heights are compared with experimental data. Favorable comparisons with experimental measurements are demonstrated.

• Transactions of the Korean Society of Mechanical Engineers B
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• 제33권8호
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• pp.589-595
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• 2009

The instability wave formed near nozzle region grows to vortex with large scale in downstream region of spray. It plays an important role in the fuel-air mixing, combustion process and engine exhaust emissions in direct injection diesel engine. The objective of this study is to analyze effect of variant parameters (injection pressure, ambient gas density, etc.) and fuel properties on spray instability near nozzle region. Spray structure near nozzle region was investigated using a magnification photograph. A pulsed Nd-YAG laser was used as a light source, and image was taken by CCD camera. The following conclusions are drawn from this experimental analysis. In low ambient density, the effect of fuel properties on spray instability near nozzle region is dominant. In high ambient density, the effect of ambient gas on spray instability near nozzle region is dominant. High jet velocity has strong influence on spray instability.

• Transactions of the Korean Society of Mechanical Engineers B
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• 제31권2호
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• pp.109-115
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• 2007

Airframe-integrated Scramjet engines of NASA Langley type consist of a compressor, a combustion chamber and a nozzle. When some disturbances occur in one module of the engine, its influences are propagated to other modules. In this study, it is investigated numerically how shock waves were caused by thermal choking in one module propagate upstream and how they influence adjacent modules. The calculations are carried out in 2-dimensional supersonic viscous flow model using explicit TVD scheme in generalized coordinates. The adverse pressure gradient caused by heat addition brings about separation of the wall boundary layers and formation of the oblique shock wave that proceed to upstream. This moving shock wave formed one module blocks the flow coming into the adjacent modules, which makes the modules unstarted.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 한국소음진동공학회 2004년도 추계학술대회논문집
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• pp.866-869
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• 2004

Power transformers, air-intakes and stacks in the urban combined power plant are main noisy sources. Because of Inhabitant complaint by abnormal noise transferred from the power plant. the noise was investigated at power plant and uptown area. The result of diagnosis made the acoustic resonance phenomenon by 580Hz's combustion dynamic pressure with the standing wave mode of sound fields in exhaust passageway of gas turbine into main noise source of public complain. The abnormal noise is caused by the resonance exhaust noise transferred through stacks of power plant.

• Proceedings of the Korea Technical Association of the Pulp and Paper Industry Conference
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• 한국펄프종이공학회 2006년도 PAN PACIFIC CONFERENCE vol.2
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• pp.205-208
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• 2006

Existing gas fired burners work in the medium wave IR range at $1000^{\circ}C$ and an energy density of $200kW/m^{2}$. The patented porous burner technology reaches the short wave IR spectrum ($1450^{\circ}C$) and comes up to an energy density of $1000kW/m^{2}$. This technology is of great interest for various applications in paper industry. Speeding up existing coating lines can be realized without a major revamp of the line. Main characteristics of this new developed technology enable a better process control. In this paper the porous burner technology for paper industry is evaluated.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 한국에너지공학회 1998년도 춘계 학술발표회 논문집
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• pp.87-94
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• 1998

폭발현상(explosion phenomena)이 항상 연소(combustion)를 수반하는 것도 아니고, 연소현상이 항상 폭발적으로 일어나는 것이 아님에도 불구하고 많은 사람들은 폭발과 연소 사이에 밀접한 관계가 있는 것으로 생각하고 있다. 일반적으로 폭발이라고 하면 우선 큰 소리와 건물이나 실내의 파괴를 연상한다. 폭발 시에 발생하는 큰소리, 이른바 폭발음은 공기 중을 전파하는 압력파(blast wave)에 의한 것이고 건물이나 실내 파괴는 그들의 내부압력 상승에 의한 것이다. 그러므로 폭발현상은 압력상승과 불가분하다고 생각해도 된다. (중략)

• Proceedings of the Korean Powder Metallurgy Institute Conference
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• 한국분말야금학회 2004년도 춘계학술강연 및 발표대회 강연 및 발표논문 초록집
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• pp.21-21
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• 2004

• 한국연소학회:학술대회논문집
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• 한국연소학회 2012년도 제45회 KOSCO SYMPOSIUM 초록집
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• pp.97-99
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• 2012

A pressure-based BOIK model considering Shock to Detonation Transition(SDT) and damage due to external fragment or bullet stimuli impact on energetic materials and analytical approach for determination of free parameters are proposed. The rate of product mass fraction(${\lambda}$) consists of ignition term that represents the initiation due to shock compression and growth term that describes propagation of detonation wave and strain term representing the morphological deformation induced by external impact.

• Proceedings of the Korean Powder Metallurgy Institute Conference
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• 한국분말야금학회 2005년도 춘계학술강연 및 발표대회강연 및 발표논문 초록집
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• pp.52-52
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• 2005

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 한국추진공학회 1998년도 제10회 학술강연회논문집
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• pp.28-28
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• 1998

고주파 연소불안정은 거의 모든 로켓엔진의 개발 프로그램에서 보고되고 있으며, 이 문제의 해결을 위한 많은 연구들이 진행되어 왔다. 고주파 연소불안정은 로켓엔진 연소실 내에서의 연소와 유동변수들이 커플링되어 발생한다. 연소가스의 음향파동은 연소의 외란을 야기하며 외란된 연소는 유동변수들에 맥동에너지를 공급하는 되먹임 과정을 반복하게 된다. 결과적으로 음향파에 의한 외란의 크기, 위상 및 되먹임 과정에서의 파동에너지 감쇠량에 따라 불안정한 파동은 증폭, 유지되거나 소멸된다.