• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제35회 추계학술대회논문집
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• pp.729-732
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• 2010

본 연구는 케로신과 액체산소를 추진제로 사용하는 동축 와류형 분사기를 해석하기 위해 체계적인 물리 모델링을 수행하였다. 먼저 초임계 압력 조건에서 나타나는 실제유체의 열역학 및 전달 물성치를 계산할 수 있는 서브루틴 라이브러리를 구축하였으며, 층류 화염편 해석 코드와 연동하여 케로신 난류연소장의 국소화염구조를 해석하였다. 설계 목적에 맞는 계산 효율성을 확보하기 위해 동축 와류형 분사기는 RANS 기반의 2차원 축대칭 선회 유동으로 해석하였으며, 실험 결과가 존재하는 비연소 동축선회 제트 유동을 통해 예측정확도를 검증하였다. 실제 고압 연소를 수반하는 동축 와류형 분사기의 경우, 기존의 RANS 모델은 급격한 밀도 구배가 수반되는 선회 막 유동의 혼합층에서 과도한 난류확산을 야기하였으며, 난류모델의 수정을 위해 보다 심도 있는 연구가 필요할 것으로 판단되었다.

• 대한기계학회논문집B
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• 제21권10호
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• pp.1350-1362
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• 1997

An experimental study has been performed on vortex pairing under fundamental and subharmonic forcing with controlled initial phase differences through hot-wire measurements and a multi-smoke wire flow visualization. For the range of St$_{D}$ < 0.6, vortex pairing was controlled by means of fundamental and subharmonic forcing with varying initial phase differences. Much larger mixing rate was achieved by two-frequency forcing with a proper phase difference than one frequency forcing. As St$_{D}$ decreased, vortex pairing was limited to a narrow region of the initial phase difference between two disturbances and higher amplitudes of the fundamental and its subharmonic at the nozzle exit were required for more stable pairing. As the amplitude of the subharmonic at the nozzle exit increased for fixed St$_{D}$ and fundamental amplitude, the distribution of the subharmonic mode against the variation of the initial phase difference changed from a sine function form into a cusp-like form. Thus, vortex pairing can be controlled more precisely for the former case. For St$_{D}$ > 0.6, non-pairing advection of vortices due to the improper phase difference was sometimes observed in several fundamental forcing amplitudes when only the fundamental was applied. However, when its subharmonic was added, vortex pairing readily occurred. As the initial amplitude of this subharmonic increased, the position of vortex pairing moved upstream. This was thought to be due to the fact that the variation of the initial phase difference between the fundamental and its subharmonic has less effects on vortex pairing in the region of fundamental-only vortex pairing.pairing.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.680-685
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• 2008

The ejector is a simple device which can transport a low-pressure secondary flow by using a high-pressure primary flow. In general, it consists of a primary driving nozzle, a mixing section, and a diffuser. The ejector system entrains the secondary flow through a shear action generated by the primary jet. Until now, a large number of researches have been made to design and evaluate the ejector systems, where it is assumed that the ejector system has an infinite secondary chamber which can supply mass infinitely. However, in almost all of the practical applications, the ejector system has a finite secondary chamber implying steady flow can be possible only after the flow inside ejector has reached an equilibrium state after the starting process. To the authors' best knowledge, there are no reports on the starting characteristics of the ejector systems and none of the works to date discloses the detailed flow process until the secondary chamber flow reaches an equilibrium state. The objective of the present study is to investigate the starting process of an ejector-diffuser system. The present study is also planned to identify the operating range of ejector-diffuser systems where the steady flow assumption can be applied without uncertainty. The results obtained show that the one and only condition in which an infinite mass entrainment is possible is the generation of a recirculation zone near the primary nozzle exit. The flow in the secondary chamber attains a state of dynamic equilibrium at this point.

• 암석학회지
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• 제1권2호
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• pp.91-103
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• 1992

Eruptive mechanisms and processes at Udo tuff cone can be inferred from indicative characters of products, bedforms and lithofacies, and ring faults. In terms of bedforms and lithofa-cies in particular, massive lapilli tuff beds and chaotic lapilli tuff beds are derived from subaerial falls of aggregated tephra of wet tephra finger jets, occurring dominantly at the lower sequences of proximal part at the tuff cone. Crudely stratified lapilli tuff are derived from subaerial falls of slightly aggregated tephra of less wet tephra finger jets, whereas reversely graded lapilli tuff beds are from slightly disaggregated subaerial falls of continuous uprush. Both beds frequently occur in the middle sequences at proximal and near medial part of the tuff cone. Block and lapilli tephra lenses, ash-coated lapilli tephra beds(lenses) and thin-bedded tuff beds are derived from extremely disaggregated subaerial falls of dry tephra in the continuous uprush, frequently occurring at the upper sequences of medial part at the tuff cone. Udo tuff cone is a basaltic volcano emergent through the sea water surface while water could flood across or into the vent area. Emergence of the tuff cone was from the type-Surtseyan eruption characterized by earlier tephra finger jets and later continuous uprush columns of tephra with copious volumes of steam. Explosions began when boiling of wter produced a bubble column reducing the hydrostatic pres-sure, allowing exsolution of gases from the magma. This expansion of magma into a vesiculating froth fragmented the magma and permitted mixing of magma and water so that a more vigorous generation of steam could proceed. Tephra finger jetting explosions continued to build the crater rims, then remove water from the vent that their deposits flowed like slsurries until the continuous uprush explosion ensued. Continuous uprush explosions were associated with most rapid accumula-tion of tephra. The increasing volume rate led to partial removal of water from the vent area by the newly tephra ring so that more vigorous activity could be attended by a reducing water supply. This might restrain surplus of cold water entering the vent and thus enhance the vigour of the eruption by allowing optimal heat exchange. Eventually the crater became so deep and unsuported that piecemeal sliding, or massive subsidence on indipping ring faults, filled and closed the vent, and the cycle of explosions and collapse began anew.

• Geomechanics and Engineering
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• 제34권5호
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• pp.491-505
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• 2023

The practical usage of underground space and demand for vehicular tunnels necessitate the construction of non-circular wide rectangular tunnels. However, constructing large tunnels in soft clayey soil conditions with no ground improvement can lead to excessive ground deformations and collapse. In recent years, in situ ground improvement techniques such as jet grouting and deep cement mixing are often utilized to perform cement-stabilisation around the tunnel boundary to prevent large deformations and failure. This paper discusses the stability characteristics and failure behaviour of a wide rectangular tunnel in cement-treated soft clays. First, the plane strain finite element model is developed and validated with the results of centrifuge model tests available in the past literature. The critical tunnel support pressures computed from the numerical study are found to be in good agreement with those of centrifuge model tests. The influence of varying strength and thickness of improved soil surround, and cover depth are studied on the stability and failure modes of a rectangular tunnel. It is observed that the failure behaviour of the tunnel in improved soil surround depends on the ratio of the strength of improved soil surround to the strength of surrounding soil, i.e., q_ui/q_us, rather than just q_ui. For low q_ui/q_us ratios,the stability increases with the cover; however, for the high strength improved soil surrounds with q_ui >> q_us, the stability decreases with the cover. The failure chart, modified stability equation, and stability chart are also proposed as preliminary design guidelines for constructing rectangular tunnels in the improved soil surrounded by soft clays.

• 한국추진공학회지
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• 제2권2호
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• pp.56-63
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• 1998

본 논문에서는 주유동의 난류강도 변화에 따른 복합각도로 분사되는 단일 막냉각홀 주위에서의 국소 열/물질전달계수 특성을 살펴보기 위하여 실험을 수행하였다. 단일 막냉각홀 시편은 평면에 대하여 $30^{\cire}$의 경사각을 가지고 있으며, 횡방향으로는 주유동에 대해 $45^{\cire}$의 각도로 분사하여 복합각도 분사시 주유동의 난류강도 변화에 따른 효과를 살펴보았다. 또한 막냉각제트의 분사율을 0.5에서 2.0까지 변화시켜가며, 주유동의 높은 난류강도조건에서 분사율 변화시 막냉각홀 주위의 열/물질전달특성에 미치는 효과를 살펴보았다. 주유동의 난류강도를 변화시키기 위하여 막냉각홀 상류에 난류발생격자를 설치하였다. 격자를 설치하지 않은 경우, 주유동의 난류강도는 0.5%이며, 난류발생격자의 종류 및 설치위치를 달리하여 난류강도를 3%에서 10%까지 변화시켜가며 실험하였다. 막냉각홀 주위에서 국소적인 열/물질전달계수 값을 얻기 위하여 물질전달 실험방법인 나프탈렌 승화법을 사용하였다. 주유동의 난류강도가 낮은 경우 분사홀 주변에서 막냉각제트 혹은 주유동에 의한 열/물질전달 촉진영역이 뚜렷한 경계를 갖지만, 난류강도가 증가하면서 전 영역에 걸쳐 열/물질전달이 촉진되었으며 주유동과 막냉각제트의 활발한 혼합작용으로 인해 영역의 구분이 점차 소멸되었다. 또한 주유동의 높은 난류강도 효과는 막냉각제트의 분사율이 높은 경우 뚜렷이 나타났다.

• 한국터널지하공간학회 논문집
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• 제17권2호
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• pp.141-151
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• 2015

터널굴착의 효율성 증진 및 굴착시 발생하는 진동 저감을 위해 연마재 투입형 워터젯 시스템을 이용한 새로운 형태의 암반 굴착 방식이 개발되어 적용 중에 있다. 연마재 투입형 워터젯 시스템을 이용한 암반 굴착 방식에 있어서, 적절한 양의 연마재를 투입하는 것은 절삭 성능뿐만 아니라 전체 공정의 경제성 향상을 위해서도 매우 중요하다. 본 연구에서는, 다양한 공정 변수들 중 터널 굴착용 워터젯 시스템에서 특히 중요한 공정 변수들인 기하학적 변수(연마재 탱크(또는 호퍼) 높이, 연마재 투입관의 구배, 연마재 투입관의 길이, 연마재 투입관의 굴곡도), 연마재 변수(연마재 입자 크기), 젯 에너지 변수(수압, 유량)이 연마재 투입량 및 연마재가 믹싱 챔버 내로 흡입될 때 발생하는 흡입 압력에 미치는 영향을 규명하기 위하여 다양한 조건에서 실험을 수행하고 그 결과를 분석하였다. 또한, 실험적 연구를 통하여 연마재 투입량이 절삭 성능에 미치는 영향을 논의하였다. 본 연구 결과를 바탕으로 주요 공정 변수들을 조절하여 적절한 연마재 투입량을 유지하면 터널 굴착용 워터젯의 절삭 성능을 극대화할 수 있을 것으로 기대된다.

• 대한토목학회논문집
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• 제32권2A호
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• pp.123-130
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• 2012

증기를 발생시켜 터빈(turbine)을 회전시키는 화력 및 원자력 발전 계통에서 냉각시설은 필수적인 구조물이며, 냉각수 순환 계통은 일반적으로 해수를 취수하여 발전소 내의 복수기까지 유입시켜 증기와 열 교환 후 다시 외해로 배출시키는 형태를 취하고 있다. 최근 냉각수 취 배수 방식을 표층 취 배수 방식이 아닌 심층 취 배수 방식으로 변경하고 있는데, 기존 원전의 재순환 온도에 대한 영향을 최소화 하고, 온배수 방류시 밀도차로 인한 부력으로 온배수 혼합효과를 높여 온배수에 의한 환경피해 범위를 최소화하기 위해서이다. 특히, 하절기에 저층의 저온 냉각수를 취수할 수 있다는 이점 때문에 향후 계획되는 발전소들도 심층 취 배수 방식을 도입할 것으로 예상된다. 본 연구에서는 원자력 발전소의 냉각시설 중 심층 취 배수 구조물의 입구 주변을 3차원 전산유체역학 코드인 $FLOW-3D^{(R)}$로 모사하여 그 흐름특성을 분석하였다. 취수구(intake)의 경우 연직취수 조건에서 유속 덮개(Velocity cap), 배수구(diffuser)의 경우 방류수의 분사방향에 변화를 주어 모의하였으며, 그 결과 취수구의 경우 유속덮개에 의한 연직 유속성분의 현저한 감소로 인한 어류 유입영향을 최소화할 수 있을 것으로 판단되며, 배수구 희석효과는 Jirka 및 Harleman이 제시한 2차원 온배수 프룸(frume)과 잘 일치 하는 것으로 나타났다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제36회 춘계학술대회논문집
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• pp.1-2
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• 2011

Hybrid rockets have lately attracted attention as a strong candidate of small, low cost, safe and reliable launch vehicles. A significant topic is that the first commercially sponsored space ship, SpaceShipOne vehicle chose a hybrid rocket. The main factors for the choice were safety of operation, system cost, quick turnaround, and thrust termination. In Japan, five universities including Hokkaido University and three private companies organized "Hybrid Rocket Research Group" from 1998 to 2002. Their main purpose was to downsize the cost and scale of rocket experiments. In 2002, UNISEC (University Space Engineering Consortium) and HASTIC (Hokkaido Aerospace Science and Technology Incubation Center) took over the educational and R&D rocket activities respectively and the research group dissolved. In 2008, JAXA/ISAS and eleven universities formed "Hybrid Rocket Research Working Group" as a subcommittee of the Steering Committee for Space Engineering in ISAS. Their goal is to demonstrate technical feasibility of lowcost and high frequency launches of nano/micro satellites into sun-synchronous orbits. Hybrid rockets use a combination of solid and liquid propellants. Usually the fuel is in a solid phase. A serious problem of hybrid rockets is the low regression rate of the solid fuel. In single port hybrids the low regression rate below 1 mm/s causes large L/D exceeding a hundred and small fuel loading ratio falling below 0.3. Multi-port hybrids are a typical solution to solve this problem. However, this solution is not the mainstream in Japan. Another approach is to use high regression rate fuels. For example, a fuel regression rate of 4 mm/s decreases L/D to around 10 and increases the loading ratio to around 0.75. Liquefying fuels such as paraffins are strong candidates for high regression fuels and subject of active research in Japan too. Nakagawa et al. in Tokai University employed EVA (Ethylene Vinyl Acetate) to modify viscosity of paraffin based fuels and investigated the effect of viscosity on regression rates. Wada et al. in Akita University employed LTP (Low melting ThermoPlastic) as another candidate of liquefying fuels and demonstrated high regression rates comparable to paraffin fuels. Hori et al. in JAXA/ISAS employed glycidylazide-poly(ethylene glycol) (GAP-PEG) copolymers as high regression rate fuels and modified the combustion characteristics by changing the PEG mixing ratio. Regression rate improvement by changing internal ballistics is another stream of research. The author proposed a new fuel configuration named "CAMUI" in 1998. CAMUI comes from an abbreviation of "cascaded multistage impinging-jet" meaning the distinctive flow field. A CAMUI type fuel grain consists of several cylindrical fuel blocks with two ports in axial direction. The port alignment shifts 90 degrees with each other to make jets out of ports impinge on the upstream end face of the downstream fuel block, resulting in intense heat transfer to the fuel. Yuasa et al. in Tokyo Metropolitan University employed swirling injection method and improved regression rates more than three times higher. However, regression rate distribution along the axis is not uniform due to the decay of the swirl strength. Aso et al. in Kyushu University employed multi-swirl injection to solve this problem. Combinations of swirling injection and paraffin based fuel have been tried and some results show very high regression rates exceeding ten times of conventional one. High fuel regression rates by new fuel, new internal ballistics, or combination of them require faster fuel-oxidizer mixing to maintain combustion efficiency. Nakagawa et al. succeeded to improve combustion efficiency of a paraffin-based fuel from 77% to 96% by a baffle plate. Another effective approach some researchers are trying is to use an aft-chamber to increase residence time. Better understanding of the new flow fields is necessary to reveal basic mechanisms of regression enhancement. Yuasa et al. visualized the combustion field in a swirling injection type motor. Nakagawa et al. observed boundary layer combustion of wax-based fuels. To understand detailed flow structures in swirling flow type hybrids, Sawada et al. (Tohoku Univ.), Teramoto et al. (Univ. of Tokyo), Shimada et al. (ISAS), and Tsuboi et al. (Kyushu Inst. Tech.) are trying to simulate the flow field numerically. Main challenges are turbulent reaction, stiffness due to low Mach number flow, fuel regression model, and other non-steady phenomena. Oshima et al. in Hokkaido University simulated CAMUI type flow fields and discussed correspondence relation between regression distribution of a burning surface and the vortex structure over the surface.