• Journal of the Korean Society of Propulsion Engineers
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• v.22 no.2
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• pp.96-107
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• 2018

Flow analysis using computational fluid dynamics was conducted to investigate the effect of the igniter flame caused by the gap between the igniter and the propellant grain in a solid rocket motor. Two propellant grain types were assumed; namely cylinder type (1 mm, 3 mm, and 5 mm gap) and the slot type. The slot type had two igniter hole locations. One was located at the small gap of the propellant grain, and the other one was located at the large gap. In the case of the cylinder type, the pressure in the igniter zone was higher with a thinner gap. Additionally, in the case of the cylinder type, the pressure difference between the igniter installed zone and the free volume was also higher as the gap became lower. The cylinder types were affected by the gap distance, but the slot types were not. Moreover, the results of the slot types were similar to the 5-mm gap case of the cylinder type.

• Journal of the Korean Society of Propulsion Engineers
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• v.21 no.6
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• pp.103-109
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• 2017

An increase in acoustic energy in a combustion chamber coupled with heat fluctuations from flame results in the occurrence of combustion instability. The assessment of combustion stability requires the prediction of acoustic energy variation by understanding the acoustical characteristics of flow boundaries in a combustion chamber. The present paper discusses about the characteristics of acoustic impedances at boundaries in terms of Strouhal number and summarizes theoretical analyses on the acoustic characteristics of injector-head-like configurations. Also, the details of the two-microphone measurement technique have been presented.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• v.y2005m4
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• pp.364-367
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• 2005

A series of computational simulations have been carried out for non-reacting and reacting flows in channel-type and divergent scramjet combustor configurations with and without a cavity. Transverse injection of hydrogen is considered with the injection pressure varying from 0.5 to 1.5 MPa. The detailed resolution of the oscillatory flow and flame dynamics are captured at sufficient scale to identify the underlying physical mechanisms, and the role of combustor configuration, cavity and amount of heat addition could be understood.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 1993.04b
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• pp.23-27
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• 1993

스테인리스강은 내식성, 내열성, 내산화성이 좋으므로 화학산업, 의학용기, 고정밀 산업 등에서 많이 사용되고 있다. 스테인리스강은 열전도율이 낮고 용융물의 점성이 크고 가공경화가 심하기 때문에 인코넬 티탄합금 등과 함께 난삭재로 알려져 있다. 스테인리스강의 고합금강을 사용한 기계가공은 공구의 마모가 심하게 일어나므로 가 공이 어렵다. 화염절단(Flame dutting)도 합금물의 버닝(burning)현상을 막는 성질 때문에 잘쓰이지 않고 플라 즈마-아크(plasma-arc) 절단은 수중에서 이루어질 경우 절단끝이 산화되지 않는 좋은 절단면을 얻을 수 있으나 수중에서 사용해야 하는 어려움이 있다. 레이저를 이용한 가공은 절단폭이 작아 재료의 손실이 적으며 복잡한 형상의 절단도쉽고 공구의손실이 없는등 많은 장점이 있어서 사용이 증가하고 있다. 본 연구에서는 스테인리스 강의 절단메커니즘에대한 이해를 돕기 위해 절단가공에 큰 영향을 끼치는 레이저 출력, 절단속도, 절단가스의 압력, 재질, 절단두께를 절단변수로채택하여 절단을 수행하였다. 절단결과를 비교 검토하여 절단변수가 절단에 미치는 영향을 분석하였고 최적의 절단을 얻는 가공조건을 제시하였다.

• 한국연소학회:학술대회논문집
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• 2005.10a
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• pp.314-319
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• 2005

In this study, the combustion characteristics were investigated with the variation of design factors on multiple slit gas burner. The design factors consist of slit height, width, spacing, and inner length. The combustion characteristics were made analysis of the CO emission and NOx emission by using CO analyzer and NOx analyzer. The lower perimeter to area and the narrow spacing extends the lift-flame limit. The CO emission increases with the increasing perimeter to area ratio at the same condition. The NOx emission is found to be less significant with the port perimeter to area ratio. The flame interference might highly depend on the spacing and port perimeter to area ratio, and it also affects the burner performance.

• 한국연소학회:학술대회논문집
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• 2012.04a
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• pp.43-46
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• 2012

The oxygen concentration of primary oxidizer is decided under 10% due to flammable risk. It can be a spontaneous combustion inside burner or tube if the excess oxygen is added to primary oxidizer in Oxy-PC burner. In this case, the rest oxygen which can not be injected to primary oxidizer should be injected to another port. If added it to a second oxidizer, the ignition is unstable at outlet of burner. Accordingly an extra lancing port is needed to insert into the burner unlike other common air mode. And the flame formation and combustion characteristic differ from lancing port position. Therefore we observed flame formation which has stable combustion characteristic according to the shape and position of lancing port.

• 한국연소학회:학술대회논문집
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• 2002.11a
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• pp.71-79
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• 2002

The characteristics of the catalytically supported combustion with Pd and Pd/Pt based catalyst using the bench-scaled high pressure combustor have been investigated up to 5atm. This study aimed to investigate combustion characteristics of the stable flame attached to the exit of catalyst bed and NOx emissions with respect to the position of axial and radial direction in the combustor. NOx emissions were increased along the axial distance after the catalyst bed exit and radially decreased from the center to the wall of the combustor. At the higher pressure, the NOx emission decreased slightly due to the lower flame temperature in the combustor at the high pressure.

• Journal of the Korean Society of Propulsion Engineers
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• v.6 no.2
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• pp.29-36
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• 2002

Experiments have been performed to investigate the effect of secondary venturi tip angle on flow and spray characteristics in gas turbine combustor with a swirl cup assembly. Three variations of secondary venturi tip angle are made: converging, straight and diverging angles. It is found that the variation of venturi tip angle results in the significant changes of flow and spray characteristics in gas turbine combustors, such as the size and location of recirculation zones. drop size and mass distribution affecting combustion efficiency and NOx emissions. In diverge case, central toroidal recirculation zone(CTRZ) exists near the exit, which is known to be beneficial for flame stability. But in converge case, the finest SMD distribution and uniform mass distribution are found and CTRZ is longer than other cases. Consequently, high combustion efficiency and low pollutant emission are expected in converge case.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.11a
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• pp.49-53
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• 2009

The paper presents the results of the experimental study about flow discharge characteristics of double swirl coaxial injectors for a liquid rocket engine. Flow discharge characteristics of injectors become one of critical design issues for LRE combustion devices. Tap water and liquid oxygen/kerosene were used for ambient and hot firing tests, respectively. A combustion discharge coefficient varies depending on a mixture ratio and a recess ratio, and magnitudes of the variations are different with respect to injector shapes and operating conditions. The variation of a combustion discharge coefficient with a LOx injector is considered to result from flame structure changes due to physical property changes.

• Journal of the korean Society of Automotive Engineers
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• v.8 no.2
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• pp.13-21
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• 1986

점차 엄격해지는 요구조건을 만족시켜 주기 위해서는 승용차용 엔진의 실제특성과 운전특성을 지 배하는 설계변수의 조절은 불가피하며, 그중에서도 엔진의 핵심부인 연소질의 설계는 가장 중요 하다. 부분 부하에서의 SI기관의 연료경제성을 향상시키는 가장 좋은 방법이 압축비를 상승시 키는 것이므로, 앞으로의 여소실은 고압축비에서도 옥탄가가 높은 연료를 요구하는 성향을 낮 추는 특성을 갖고 있어야 한다. 새로운 엔진의 향상을 최적화하기 위하여는 quench area의 크 기와 위치 그리고 적절한 quench distance의 성질이 중요하며, 또한 연소실의 소형화, 스파크 플러크의 위치, 표면적/체적의 비 그리고 화염전파거리등도 고려에 넣어야 한다. 승용차용 엔진의 요구조건은 연소실을 피스톤 크라운에 위치시키는 용이한 방법을 통하여 해결될 수 있으며, 이 러한 형상의 연소실은 실린더 헤드에 장치한 연소실과 비교하여 다음과 같은 장점을 갖고 있다. - 스파크 플러그 주변에 연소실을 배치하기 쉽다. - 연소실 내에 quench area의 설정이 자유롭다. - 연소실 layout의 개조없이 압축비의 설정이 자유롭다. - 연소실의 조합이 간단하다. - 실린더벽으로의 열손실이 감소되어 열효율이 증대된다. - 공연비의 희박가능한계가 크다. - EGR성능이 향상되어 NOx 의 배출과 연료소비율이 감소된다. - 필요하다면 연소실실 또는 직접분사식 Diesel 기관으로서의 개조가 간단하다. 만약 생산단가가 크게 상승하지 않는다면, NOx의 배출과 연료소비율이 작으면서도, 비출력이 큰 4-밸브 연소실이 실용화 될 전망이다.