• 한국추진공학회지
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• 제17권5호
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• pp.86-94
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• 2013

로켓의 연소불안정과 관련되어 분사기의 동특성을 연구하는 일은 중요하다. 와류형 분사기의 동특성에 대해서는 많은 연구가 이루어졌지만 충돌형 분사기의 동특성에 대해서는 알려진 바가 거의 없다. 따라서 본 연구에서는 충돌형 분사기의 동특성을 규명하기 위해 이에 관한 실험을 수행하였으며 동적거동을 생성시키기 위해 특별히 제작된 압력섭동기(mechanical pulsator)가 사용되었다. 가진주파수와 매니폴드 압력의 여러 조건 하에서 게인(gain)과 위상차(phase difference)를 분석하였고 주파수는 5, 10, 15 Hz의 낮은 영역에 맞춰졌다. 제트 속도를 결정하기 위한 방법에 대해 논의하였으며 실험과정 중에 나타난 특정현상이 클라이스트론(Klystron) 효과와 관련이 있는 것으로 판단되어 이에 대해 고려하였다.

• 한국화재소방학회논문지
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• 제22권3호
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• pp.258-264
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• 2008

본 논문에서는 산불의 한 형태인 지표화의 체계적인 연구를 위해 열량분석과 연소특성에 관한 실험방법과 측정 시스템을 제안하여 향후 산불 관련 연구에 있어서 이를 활용하고자 한다. 또한 제안된 방법과 시스템의 효용성을 나타내고자 부분적인 결과를 논문에 제시 하였다. 이를 위하여 지표화의 대표적인 연소 물질인 침엽수종과 활엽수종 낙엽을 선정하여 밀도 및 시료의 용기 크기를 변화시켜 가며 실험하였다. 열량분석은 통상 사용되는 분석기기 중 열중량 분석기(TGA : Thermogravimetric Analyzer), 연소열 측정장치(Oxygen Bomb Calorimeter)를 이용하여 분석하였으며, 연소특성은 기존의 이론적 모델로 가장 잘 알려져 있는 Pool fire모델에 따른 모의 연소실험을 통하여 지표화 상부의 열 유체속도, 연소온도, 화염 높이에 따른 열방출 속도, 연소 질량감소 속도 둥을 측정하여 분석하였다. 언급된 변수들은 지표화의 위험성 및 산불확산 예측에 기초 자료로 사용할 수 있다.

• 한국수소및신에너지학회논문집
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• 제29권2호
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• pp.219-225
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• 2018

This study was carried out to investigate the injection characteristics of 800 kPa compressed natural gas compressed natural gas (CNG) injector developed in Korea. The CNG injector with multi-holes, employed in this experiment, was designed to inject CNG in the manifold at high pressure of 800 kPa. The spray macroscopic visualization test was carried out via Schlieren photography to study fuel-air mixing process. The fundamental spray characteristics, such as spray penetration, spray cone angle and spray velocity, were evaluated in the constant volume combustion chamber (CVCC) with varying the constant back pressure in CVCC from 0 to 1.8 bar. For the safety reason, nitrogen ($N_2$) and an acetone tracer were utilized as a surrogate gas fuel instead of CNG. The surrogate gas fuel pressures were controlled at 3, 5.5, and 8 bar, respectively. Injection durations were set at 5 ms throughout the experiment. The simulating events of the low engine speed were arranged at 1,000 rpm. The spray images were recorded by using a high-speed camera with a frame rate of 10,000 f/s at $512{\times}256pixels$. The spray characteristics were analyzed by using the image processing (Matlab). The results showed the significant difference that higher injection pressure had more effect on the spray shape than the lower injection pressure. When the injection pressure was increased, the longer spray penetration occurred. Moreover, the linear relation between speed and time are dependent on the injection pressure as well.

• 한국항공우주학회지
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• 제35권8호
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• pp.699-705
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• 2007

최근의 실험 결과를 통해 하이브리드 로켓 연료의 표면에 연소가 진행되지 않은 채 남아있는 고립된 부분들이 존재함을 확인하였다. 이러한 불규칙적인 spot은 연료의 기화로 인한 분출유동(blowing velocity)과 산화제의 유동 사이에서 발생하는 경계층 교란에 의한 현상인 것으로 여겨진다. 본 연구에서는 22,500의 높은 Reynolds수와 벽면분출 현상을 효과적으로 처리할 수 있도록 LES 기법을 이용하여, 연료 표면 근처의 난류 유동 및 열전달 특성을 해석하였다. 비록 원형 그레인 아닌 단순채널 형상을 고려하였으며 화학반응이 없는 경우의 난류유동을 해석하였으나, 연료 표면에서 발생하는 불규칙한 spot의 발생은 경계층과 분출되는 유동이 상호 간섭함으로써 난류구조들의 기구학적 특성을 변경시키기 때문인 것으로 추측되는 결과들을 얻을 수 있었다.

• 한국연소학회지
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• 제17권1호
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• pp.48-57
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• 2012

Laminar lifted propane coflow-jet flames diluted with nitrogen were experimentally investigated to determine heat-loss-related self-excitation regimes in the flame stability map and elucidate the individual flame characteristics. There exists a critical lift-off height over which flame-stabilizing effect becomes minor, thereby causing a normal heat-loss-induced self-excitation with O(0.01 Hz). Air-coflowing can suppress the normal heat-loss-induced self-excitation through increase of a Peclet number; meanwhile it can enhance the normal heat-lossinduced self-excitation through reducing fuel concentration gradient and thereby decreasing the reaction rate of trailing diffusion flame. Below the critical lift-off height. the effect of flame stabilization is superior, leading to a coflow-modulated heat-loss-induced self-excitation with O(0.001 Hz). Over the critical lift-off height, the effect of reducing fuel concentration gradient is pronounced, so that the normal heat-loss-induced self-excitation is restored. A newly found prompt self-excitation, observed prior to a heat-loss-induced flame blowout, is discussed. Heat-loss-related self-excitations, obtained laminar lifted propane coflow-jet flames diluted with nitrogen, were characterized by the functional dependency of Strouhal number on related parameters. The critical lift-off height was also reasonably characterized by Peclet number and fuel mole fraction.

• 한국분무공학회지
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• 제1권2호
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• pp.16-23
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• 1996

In case of a high-speed D.I. diesel engine. the injected fuel spray is unavoidable that the impinging on the wall of piston cavity and in this case the geometry of piston cavity has a great influence on the atomization structure and air flow fields. In the field of combustion and in many other spray applications, there are clear evidence of correlation between spray structure and emission of pollutants. Ordinary, the combustion chamber of driving engine have unsteady turbulent flow be attendant on such as the change of temperature, velocity and pressure. So the analysis of spray behavior is difficult. In this study, a single spray was impinged on each cavity wall at indicated angle in a quiescent atmosphere at room temperature and pressure, as being the simplest case, and 3 types of piston cavity such as Dish, Toroidal and Re-entrant type was tested for analyzing the influence of cavity geometry. And hot wire probe was used for analyze non-steady flow characteristics of impinging spray, and to investigate the behavior of spray, the aspects of concentration c(t), standard deviation $\sigma(t)$ and variation factor (v.f.) was measured with the lapse of time.

• 한국추진공학회지
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• 제16권1호
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• pp.9-15
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• 2012

하이브리드 연소실의 국부 압력과 속도변화를 고려하는 비정상 내탄도 해석모델을 제안하고 이를 바탕으로 연소실 내 국부영역에서 내탄도 특성인자의 변화를 도출하였다. 해석 모델 검증을 위하여 연소실 전후단의 압력을 측정한 실험결과와 해석결과를 비교하여 실험과 해석결과가 유사함을 확인하고 연소 효율을 평가 하였다. 하류방향으로 산화제 유량이 변화하므로 이에 따른 연소실 국부영역의 압력, 온도, 연료의 후퇴율 및 연소가스의 유속 변화를 정량적으로 고찰하였다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 추계학술대회
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• pp.490-495
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• 2003

In steel-making process of iron and steel industry, the purity and quality of steel can be dependent on the amount of CO contained in the molten metal. Recently, the supersonic oxygen jet is being applied to the molten metal in the electric furnace and thus reduces the CO amount through the chemical reactions between the oxygen jet and molten metal, leading to a better quality of steel. In this application, the supersonic oxygen jet is limited in the distance over which the supersonic velocity is maintained. In order to get longer supersonic jet propagation into the molten metal, a supersonic coherent jet is suggested as one of the alternatives which are applicable to the electric furnace system. It has a flame around the conventional supersonic jet and thus the entrainment effect of the surrounding gas into the supersonic jet is reduced, leading to a longer propagation of the supersonic jet. In this regard, gasdynamics mechanism about why the combustion phenomenon surrounding the supersonic jet causes the jet core length to be longer is not yet clarified. The present study investigates the major characteristics of the supersonic coherent jet, compared with the conventional supersonic jet. A computational study is carried out to solve the compressible, axisymmetric Navier-Stokes equations. The computational results of the supersonic coherent jet are compared with the conventional supersonic jets.

• 한국자동차공학회논문집
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• 제4권3호
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• pp.211-219
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• 1996

In a small high-speed D. I. diesel engine, the injected fuel spray into the atmosphere of the high temperature is burnt by go through the process of break up, atomization, evaporation and process of ignition. These process are important to decide the emission control and the rate of fuel consumption and out put of power. Especially, in the case of injected fuel spray impinging on the wall of piston cavity, the geometry of piston cavity gives great influence the ignitability of injected fuel and the flame structure. Ordinary, the combustion chamber of driving engine have unsteady turbulent flow be attendant on such as the change of temperature, velocity and pressure. So the analysis of spray behavior is difficult. In this study, the spray was impinged on the wall of 3 types of piston cavity such as Dish, Toroidal, Re-entrant type, in order to analyze the combustion process of impinging spray precisely and systematically. And hot wire probe was used for analyze non-steady flow characteristics of impinging spray, and to investigate the behavior of spray, the aspects of concentration c(t), standard deviation σ(t) and variation factor(vf) was measured with the lapse of time.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제34회 춘계학술대회논문집
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• pp.14-17
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• 2010

7개 스월 인젝터 연소기의 스월 방향에 따른 유동 특성을 파악하기 위하여 3차원 Large Eddy Simulation(LES)을 수행하였다. 해석에 이용된 연소기 모델은 Georgia 공대 Aerospace Combustion Laboratory의 LRE combustor를 이용하였으며, 경계 조건은 실험에서 얻어진 값을 적용하였다. 7개 인젝터의 스월 방향을 모두 동일한 방향으로 설정하였을 경우, 스월 유동간의 간섭이 증가하게 되고, 연소실 벽면에서 강한 원주방향의 속도 분포가 형성되는 것을 관찰하였다. 또한 연소실 내 압력변동폭은 인젝터의 스월 방향을 상반되게 설정하였을 때보다 현저히 증가한 것을 확인하였다.