• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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• pp.451-455
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• 2017

ZPP와 THPP 화약의 압력 카트리지가 밀폐용기에 장착되어 연소될 때의 현상을 반응성 오일러리안-라그랑지안 이상 유동 해석 코드를 통해 모사 하였다. ZPP와 THPP는 압력 카트리지 내에서 boron nitride 판으로 격리되어있고, ZPP만 열선에 의해 직접 점화되기 때문에 THPP의 연소지연효과가 발생할 가능성이 높다. 실험을 통한 THPP의 점화지연 측정은 힘들기 때문에 기존의 연구를 통해 검증된 수치해석 코드를 통해 점화지연에 대한 케이스 스터디를 수행하고 현상학적 분석을 수행하였다. 해석 결과 THPP의 점화지연 정도에 따라 초기 충격파의 강도가 변하여 압력선도의 초기 피크특성 뿐만 아니라 주파수에도 영향을 미친다는 것을 알 수 있었다.

• 한국연소학회지
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• 제18권3호
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• pp.44-53
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• 2013

In this study, the economic evaluation for imported coals was conducted for power plant based on thermo-dynamical performance analysis. The number of coal types considered was 1,755 imported by five power generation companies in Korea during the 2010-2012. The higher heating value (HHV) of the coals ranged 4,000-6,500 kcal/kg, mostly sub-bituminous. The 1D thermo-dynamical performance modeling was performed for a 500 MWe standard power plant using PROATES code. It was founded that the low rank coals had negative effects on the plant efficiency mainly due to the increased heat loss by moisture, hydrogen and flue gas. Based on the performance analysis, the economic performance of the coals was evaluated. The apparent price of low-rank coals tended to be significantly lower than design coal; for example, the unit price of coal with a HHV of 4,000 kcal/kg was 57% of the reference coal having 6,080 kcal/kg. Considering the negative effects leading to a decrease in the thermal performance, heating value compensation, and increased parasite load, the corrected unit cost for the coal with 4,000 kcal/kg was 90.7% of the reference coal. Overall, the cost saving by imported coals was not high as expected.

• International Journal of Automotive Technology
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• 제6권2호
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• pp.95-105
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• 2005

Diesel engines have low specific fuel consumption, but high particulate emissions, mainly soot. Diesel soot is suspected to have significant effects on the health of living beings and might also affect global warming. Hence stringent measures have been put in place in a number of countries and will be even stronger in the near future. Diesel engines require either advanced integrated exhaust after treatment systems or modified engine models to meet the statutory norms. Experimental analysis to study the emission characteristics is a time consuming affair. In such situations, the real picture of engine control can be obtained by the modeling of trend prediction. In this article, an effort has been made to predict emissions smoke and NO$_{x}$ using cylinder combustion derived parameters and diesel particulate filter data, with artificial neural network techniques in MATLAB environment. The model is based on three layer neural network with a back propagation learning algorithm. The training and test data of emissions were collected from experimental set up in the laboratory for different loads. The network is trained to predict the values of emission with training values. Regression analysis between test and predicted value from neural network shows least error. This approach helps in the reduction of the experimentation required to determine the smoke and NO$_{x}$ for the catalyst coated filters.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제36회 춘계학술대회논문집
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• pp.89-92
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• 2011

초임계 압력 조건에서 분사된 액체추진제의 혼합 및 연소 현상을 해석하기 위해서는 열역학적 비이상성과 전달 물성치의 특이성을 예측하는 것이 선행되어야 한다. 본 연구에서는 일반화된 3차 상태방 정식(cubic EoS)을 기반으로 실제유체의 열역학/전달 물성치를 계산하는 서브루틴들을 개발하였으며, 표준 화학반응 패키지인 Chemkin과 쉽게 연동될 수 있도록 하였다. 실제유체 해석 패키지를 이용하여 기존의 층류화염편 코드를 확장하였으며, 실제 로켓엔진이 갖는 고압 연소조건하에서 케로신과 액체산소의 국소화염구조에 대한 수치해석 연구를 수행하였다.

• Advances in aircraft and spacecraft science
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• 제6권4호
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• pp.333-348
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• 2019

Low fuel regression rate is the main drawback of hybrid rocket which should be overcome. One of the improvement techniques to this problem is usage of a solid fuel grain with a complicated geometry port, which has been promoted owing to the recent development of additive manufacturing technologies. In the design of a hybrid rocket fuel grain with a complicated geometry port, the understanding of fuel regression behavior is very important. Numerical investigations of fuel regression behavior requires a capturing method of solid fuel surface, i.e. gas-solid interface. In this study, level set method is employed as such a method and the preliminary numerical tool for capturing a hybrid rocket solid fuel surface is developed. At first, to test the adequacy of the numerical modeling, the simulation results for circular port are compared to the experimental results in open literature. The regression rates and oxidizer to fuel ratios show good agreements between the simulations and the experiments, after passing enough time. However, during the early period of combustion, there are the discrepancies between the simulations and the experiments, owing to transient phenomena. Second, the simulations of complicated geometry ports are demonstrated. In this preliminary step, a star shape is employed as complicated geometry of port. The slot number effect in star port is investigated. The regression rate decreases with increasing the slot number, except for the star port with many slots (8 slots) in the latter half of combustion. The oxidizer to fuel ratio increases with increasing the slot number.

• Journal of Advanced Marine Engineering and Technology
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• 제13권4호
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• pp.63-74
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• 1989

디젤기관의 연료분사계는 연소실과 함께 디젤기관의 성능에 가장 큰 영향을 미치는 요소의 하나로 이에 대한 이해는 디젤연소 규명에 있어서 매우 중요하다. 그러나 이분사계는 발화 및 완전연소에 필요한 무화, 공기의 이용율을 증가시키는 관통성 및 분포성등의 요건뿐만 아니라 요구되는 분사율, 2차분사 그리고 분사펌프와의 결합등의 많은 문제와 연관되어 있다. 따라서 본 연구에서는 이와 같이 복잡한 디젤기관의 연료분사계를 단순화시켜서 펌프측, 노즐측 및 분사파이프측의 세부분으로 나누어 모델링하여 해석함으로써 새로운 연료분사계의 개발을 위한 기초연구자료를 구하는 것을 목적으로 하였다. 분사파이프내의 압력과 분사계의 실험을 통하여 본 모델의 타당성을 검토하였으며 각 분사계에 있어서 분사량을 최대로 하는 분사파이프직경이 존재함을 확인할 수 있었다.

• 대한기계학회논문집B
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• 제34권11호
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• pp.957-964
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• 2010

본 연구에서는 친환경 연소로서 순산소 연소의 내제한 문제점에 대하여 논의하고 있다. 그 중 DDT의 발전에 의해 발생되는 강한 압력 충격파에 의한 구조물의 손상에 대한 내용을 다루고 있다. 이를 위하여 DDT에 대해 인식시키기 위하여 기본적인 개념과 더불어 이를 발전시키는 요인들에 대해서 논의해 보았다. 그리고 순산소 연소의 DDT 발생에 의한 압력파 생성과 더불어 이에 따른 구조물 손상을 설명하기 위하여 순산소 연소를 사용하는 친환경 용융로(미분탄과 순산소 연소를 사용한 용융로) 내부의 풍구 손상을 AUTODYN hydrocode를 이용하여 모델링하였다. 이를 통하여 순산소 연소에 내제된 위험성에 대하여 살펴보았다.

• 대한기계학회논문집B
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• 제25권11호
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• pp.1594-1605
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• 2001

In this study, a numerical simulation was developed which was capable of predicting the characteristics of NO formation in pilot scale combustor adopting the air-staged burner flame. The numerical calculation was constructed by means of establishing the mathematical models fur turbulence, turbulent combustion, radiation and turbulent nitric oxide chemistry. Turbulence was solved with standard k-$\xi$ model and the turbulent combustion model was incorporated using a two step reaction scheme together with an eddy dissipation model. The radiative transfer equation was calculated by means of the discrete ordinates method with the weighted sum of gray gases model for CO$_2$and H$_2$O. In the NO chemistry model, the chemical reaction rates for thermal and prompt NO were statistically averaged using the $\beta$ probability density function. The results were validated by comparison with measurements. For the experiment, a 0.2 MW pilot multi-air staged burner has been designed and fabricated. Only when the radiation was taken into account, the predicted gas temperature was in good agreement with the experimental one, which meant that the inclusion of radiation was indispensable for modeling multi-air staged gas flame. This was also true of the prediction of the NO formation, since it heavily depended on temperature. Subsequently, it was found that the multi-air staged combustion technique might be used as a practical tool in reducing the NO formation by controlling the peak flame temperature.

• 한국항공우주학회지
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• 제34권6호
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• pp.59-66
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• 2006

액체 로켓엔진에서의 고주파 연소불안정 제어를 위한 수동 안정화 제어 기구로 음향공을 적용하여 감쇠 효과의 적합성을 검증하였다. 우선, 기본형 모델링 연소실에서 발생한 유해 공진주파수는 음향공의 동조를 통하여 효과적으로 감쇠될 수 있음을 확인 하였다. 또한, 음향공의 기하학적 형상에 따른 음향 감쇠 효과를 비교하기 위하여, 주요 설계 변수를 변화시킨 몇 가지 음향공 모델에 대해 유해 공진주파수 감쇠 효과를 정량적으로 비교, 분석하였다. 선형음향해석과 실험적 방법 모두 만족할만한 일치성을 나타내었으며, 오리피스 입구 면적이 가장 크거나 오리피스 길이가 가장 짧은 경우에서 감쇠 효과가 가장 크게 나타났다. 결론적으로 음향공을 이용한 최적의 음향공 제어를 위해서는 음향공 부피를 고려한 최적의 음향공 설계가 절대적으로 필요함을 입증한다.

• 한국안전학회지
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• 제28권3호
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• pp.39-43
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• 2013

The present study has been conducted to investigate the fire combustion properties and fire behavior of an IEEE-383 qualified flame retardant cable. The reference reaction rate and reference temperature which are commonly used in pyrolysis model of fire propagation process was obtained by the thermo-gravimetric analysis of the cable component materials. The mass fraction of FR-PVC sheath abruptly decreased near temperature range of $250{\sim}260^{\circ}C$ and its maximum reaction rate was about $2.58{\times}10^{-3}$[1/s]. For the XLPE insulation of the cable, the temperature causing maximum mass fraction change was ranged about $380{\sim}390^{\circ}C$ and it has reached to the maximum reaction rate of $5.10{\times}10^{-3}$[1/s]. The flame retardant cable was burned by a pilot flame meker buner and the burning behavior of the cable was observed during the fire test. Heat release rate of the flame retardant cable was measured by a laboratory scale oxygen consumption calorimeter and the mass loss rate of the cable was calculated by the measured cable mass during the burning test. The representative value of the effective heat of combustion was evaluated by the total released energy integrated by the measured heat release rate and burned mass. This study can contribute to study the electric cable fire and provide the pyrolysis properties for the computational modeling.