• 한국수소및신에너지학회논문집
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• 제33권6호
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• pp.776-785
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• 2022

Hydrogen combustion in modern gas-turbine engine is the cutting edge technology as carbon-free energy conversion system. Flashback of hydrogen flame, however, is inevitable and critical specially for premixed hydrogen combustion. Therefore, this experimental investigation is conducted to understand flashback phenomenon in premixed hydrogen combustion. In order to investigate flashback characteristics in premixed hydrogen (H₂)/air flame, we focus on pressure conditions and nozzle shapes. In general, quenching distance reduces as pressure of combustion chamber increases, causing flashback from boundary layer near wall. The flashback regime for reference and modified candidate configurations can broadly appear with increasing combustion chamber pressure. The later one can improve flashback-resist by compensating flow velocity at wall. Also, improved wall flow velocity profile of suggested contraction nozzle prevents entire flashback but causes local flashback at nozzle exit.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2009년도 추계학술대회 논문집
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• pp.270-275
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• 2009

Sound absorption characteristics of membrane system which are used in stadiums and arenas were investigated. Theoretical studies on acoustic properties of single and double leaf permeable membrane conducted. Also, experimental studies on sound absorption characteristics of combined membrane system that is composed of outer and inner membrane material were conducted. In this study, sound absorption characteristics of each membrane were investigated by experiments in reverberation chamber. 4 types of permeable membranes and a non-permeable membrane were used for experiments. Air space behind membrane material and tension on the membrane was varied. Sound absorption performance of permeable membrane materials was confirmed. As increasing air space behind the membrane material, sound absorption coefficient was increased. In a resonance absorption frequency band sound absorption coefficient varied more dramatically. Sound absorption characteristics were flat in mid and high frequency range and sound absorption coefficient was from 0,3 to 0,5. Also sound absorption coefficient was increased by the increment of surface density and air permeability of membrane. However, over the certain value of air permeability, sound absorption coefficient was decreased. These results can be used as design factors and method for the room acoustic design of dome-stadiums and large free-form buildings.

• Selected Papers of The Society of Naval Architects of Korea
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• 제2권1호
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• pp.29-46
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• 1994

In this paper, the effect of a skirt deformation on the responses of an Air Cushion Vehicle in waves is investigated. The air in the bag and plenum chamber is assumed to be compressible and to have a uniform pressure distribution in each volume. The free surface deformation is determined in the framework of a linear potential theory by replacing the cushion pressure with the pressure patch which is oscillating and translating uniformly. And the bag-finger skirt assumed to be deformed due to the pressure disturbance while its surface area remained constant. The restoring force and moment due to the deformation of bag-finger skirt from equilibrium shape is incorporated with the equations of heave and pitch motions. The numerical results of motion responses due to various ratios of the bag and cushion pressure or bag-to-finger depth ratios are shown.

• 한국자동차공학회논문집
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• 제6권6호
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• pp.63-71
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• 1998

In a diesel engine the phenomenon of spray impaction on a combustion chamber wall has been taken as an undesirable matter because of the deposition of fuel on the surfaces, and the subsequent slow evaporation and mixing with air resulting in unburned hydrocarbons. Therefore many researches have concentrated on avoiding fuel impaction on surfaces. On the contrary done a number of studies using spray wall impactions in a positive way, which makes the droplets smaller, changes the direction into free spaces far from the wall and also improves mixing with air. In this paper the angle variations of the impaction land sufrace prepared for the injection spray is analysed as a simulative manner. The spray dispersions, vapor distributions and flow fields are compared with impacting angle variation. The results show more angle give more vapor distribution until $15^{\circ}$.

• 한국신재생에너지학회:학술대회논문집
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• 한국신재생에너지학회 2005년도 춘계학술대회
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• pp.306-309
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• 2005

One of the most critical issues in sol id oxide fuel cell (SOFC)running on hydrocarbon fuels is the risk of carbon formation from the fuel gas. The simple method to reduce the risk of carbon formation from the reactions is to add steam to the fuel stream, leading to the carbon gasification react ion. However, the addition of steam to fuel is not appropriate for the auxiliary power unit (APU) and potable power generation (PPG) systems due to an increase of complexity and bulkiness. In this regard, many researchers have focused on so-called 'direct methane' operation of SOFC, which works with dry methane without coking. However, coking can be suppressed only by the operation with a high current density, which may be a drawback especially for the APU and PPG systems. The single chamber fuel cell (SC-SOFC) is a novel simplification of the conventional SOFC into which a premixed fuel/air mixture is introduced. It relies on the selectivity of the anode and cathode catalysts to generate a chemical potential gradient across the cell. Moreover it allows compact and seal-free stack design. In this study, we fabricated honeycomb type mixed-gas fuel cell (MGFC) which has advantages of stacking to the axial direction and increasing volume power density. Honeycomb-structured SOFC with four channels was prepared by dry pressing method. Two alternative channels were coated with electrolyte and cathode slurry in order to make cathodic reaction sites. We will discuss that the anode supported honeycomb type cell running on mixed gas condition.

• 한국수소및신에너지학회논문집
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• 제21권6호
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• pp.487-492
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• 2010

For developing a two-stroke free-piston hydrogen engine with high efficiency and low emission, determination of the scavenging type is one of the most important factor. In this research, backfire characteristics for loop scavenging were analyzed with the number of piston crevice volume and piston expansion speed. Rapid Compression Expansion Machine, RCEM was used for combustion research of the free piston $H_2$ engine in the experiment. As the results, it was shown that although backfire occurring in a loop scavenging type can be partially controled by a complete exhaust of burned gas, possibility of backfire basically exist due to the structure which piston crevice volumes contact with fresh mixture in a scavenging port. However, a loop scavenging may be considered as combustion chamber of a free piston $H_2$ engine from the point of view that backfire does not occur nearby lean equivalence ratio obtained high thermal efficiency. It was also analyzed that an advances of backfire occurrence timing with increase of the fuel-air equivalence ratio were due to promotion of flame propagation into piston crevice volumes by decrease of the quenching distance.

• Journal of Radiation Protection and Research
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• 제18권1호
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• pp.25-35
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• 1993

알파비적밀도의 이론계산방법을 개발하기 위하여 정전기방법을 이용한 분광계를 특별히 설계 제작하였다. 이 정전기분광계를 사용하여 라돈의 첫째딸핵종인 Po-218의 이온에 대해 $0.07{\sim}5.0cm^2/V\;sec$ 범위의 이동도스펙트럼을 측정하였다. 이 측정은 실리카겔, 활성탄, 분자구조의 시브필터를 통과한 탈입자가스를 사용하는 라돈쳄버내에서 수행되었다. 제작된 정전기분광계를 사용하여 쳄버내에서 새로 생성된 Po-218이온의 이동도는 $1.92cm^2/V\;s$인 것으로 측정되었다. 알파비적밀도의 이론적계산방법에 의해 얻어진 결과를 측정에 의해 얻어진 결과와 비교하였으며 측정된 스펙트럼에 관계된 불확실도를 분석하였다. 이론계산방법에 의해 얻어진 알파비적밀도와 측정된 값과의 차이에 대한 이유는 이론계산방법에서 이온의 라돈 쳄버에서의 벽제거효과를 고려하지 않았기 때문인 것으로 밝혀졌다.

• 한국해안·해양공학회논문집
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• 제32권4호
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• pp.242-251
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• 2020

본 연구에서는 직립 안벽 앞에 설치된 2차원 진동수주형 파력발전장치의 추출효율과 반사율을 규칙파와 불규칙파에 대하여 살펴보고 둘 사이의 상관관계를 조사하였다. 해석이론으로 선형포텐셜 이론에 기반을 둔 고유함수전개법을 사용하였다. 공기실이 완전 개방되었을 때 입사파에 의한 산란문제와 공기실이 닫혀 있을 때 공기실내의 변동압력에 의한 파의 방사문제를 풀어 공기실 내부의 유량을 구하고, 이를 공기실내의 공기 흐름에 대한 연속방정식에 대입하여 변동압력을 구한다. 추출파워가 최대가 되는 최적 터빈계수를 적용하여 진동수주형 파력발전장치의 최대 추출효율과 반사율을 규칙파와 불규칙파에 대하여 구하였다. 파랑에너지를 효율적으로 흡수하도록 설계된 진동수주형 파력발전장치는 동시에 반사파를 줄이는데 기여하였다.

• 한국추진공학회지
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• 제14권3호
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• pp.69-78
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• 2010

한국항공우주연구원은 2000년부터 극초음속 공기흡입식 추진기관 시험설비의 설계와 개발에 착수하여 2009년 7월 시험설비의 구축을 완료하였다. 스크램제트 엔진 시험설비(SeTF)로 명명된 본 시험설비는 자유제트 형식 시험부를 갖춘 불어내기식, 고 엔탈피 풍동으로 고압공기 공급원, 고온 공기 공급시스템, 엔진 시험부, 연료 공급시스템, 설비 제어 및 데이터 처리 시스템 그리고 배기 시스템으로 구성되어 있다. 본 논문에는 SeTF의 설계, 사양을 소개하였으며 현재 수행 중인 SeTF의 특성 파악 시험에 대한 소개 및 일부 시험 결과를 정리하였다.

• 한국해양공학회지
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• 제29권4호
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• pp.317-321
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• 2015

Many kinds of generation systems have been developed to use ocean energy. Among these, with the use of an oscillating water column (OWC) for power generation is attracting attention. The OWC-type wave power generation system converts wave energy into electricity by operating a generator turbine with the oscillating water level in a column of water. There are two ways to convert wave power into electricity using an OWC. One uses a cross-flow turbine using the water level inside the OWC. The other method uses the flow of air in a Wells turbine, which depends on the water level. An experiment was carried out using a 2-D wave tank in order to minimize the number of empirical tests. The design factors were taken from Koo et al. (2012) and the experimental environment assumed by free surface motion. This paper deals with characteristics of two types of wave energy conversion systems combine with a breakwater. One model uses an air-driven Wells turbine and a cross-flow water turbine. The other type uses a cross-flow water turbine. Wave energy converters with OWCs have mostly been studied using air-driven Wells turbines. The efficiency of the cross-flow turbine was about 15% higher than that of the other model, and the water level of the OWC internal chamber for the cross-flow water turbine and air-driven Wells turbine was less than about 40% lower than the one using only the cross-flow water turbine.