• Title/Summary/Keyword: 충돌 혼합

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Mixing Performance of Unlike Doublet Impinging Liquid Jets (이중 충돌제트의 혼합 성능 연구)

  • Jo, Yong Ho;Lee, Seong Ung;Yun, Ung Seop
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.4
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    • pp.82-91
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    • 2003
  • Experiments to investigate the mixing performance of unlike doublet impinging jets are conducted. Reynolds number of simulants used in this study rages from 1.0 to 1.5 Cold flow test is performed to investigate the hydrodynamic effect and spray of the impinging jets are collected locally and calculated by using Rupe's mixing efficiency equation. Momentum exchanges and relative velocity ratio between two jets are taken as the main parameter to represent the effect of enlargement of the orifice diameter. As diameter ratio increases, the corresponding momentum ratio where maximum mixing efficiency occurs and relative velocity at the maximum mixing efficiency ranges 0.6 to 0.7, respectively. Penetration depth can be taken as a prominent parameter to estimate the mixing efficiency.

Analysis of Electron Swarm Transport Coefficients by Collision Cross Section in Na-He Gas Mixtures (Na-He 혼합증기중에서 충돌단면적에 의한 전자군의 수송계수 해석)

  • 하성철;백수현
    • Electrical & Electronic Materials
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    • v.3 no.2
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    • pp.138-146
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    • 1990
  • 볼츠만 수송방정식에 관한 홀스타인의 식을 사용하여 온도는 273.deg.K, 상대전계의 세기가 1.leq.E/P..leq.30(V/cm Torr)인 때의 Na와 He 단일기체중을 통과하는 전자의 에너지분포함수와 수송계수를 계산하였다. 그리고 전자 이동속도의 결과치를 실험값과 비교하였으며 실험치와 계산치가 일치하도록 충돌단면적을 수정하여 계산에 적용하였다. 이러한 방법으로 Hesms 0.1[eV]-50[eV]까지 Na는 0.1[eV]-5[eV]까지의 에너지범위에서 결정된 운동량변환단면적의 값은 제한된 범위에서 Crompton 및 Nakamura의 값과 거의 일치하였다. 또한 이와 같이하여 계산된 Na와 He 단일기체의 충돌단면적을 이용하여 온도는 273.degK, 상대전계의 세기는 1.leq.E/P$_{o}$ .leq.30(V/cm Torr)의 범위에서 Na-He 혼합증기의 혼합비율을 He:Na는 99.5:0.5, 99:1, 9:1. 1:1로 변화시켜 특성에너지, 평균에너지, 전자이동속도, 전자에너지 분포함수를 게산하였다.

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Combustion Characteristics Study using Hyper-mixer in Low-enthalpy Supersonic Flow (하이퍼 혼합기를 사용한 저엔탈피 초음속 유동장 내연소 특성 연구)

  • Kim, Chae-Hyoung;Jeung, In-Seuck
    • Journal of the Korean Society of Propulsion Engineers
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    • v.17 no.6
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    • pp.75-80
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    • 2013
  • In this study, a forced ignition method with a plasma jet torch is studied in Mach 2 laboratory scaled wind-tunnel. The hyper-mixer is used as a mixer. For two normal injection cases, the one is collided against a wedge plate of the hyper-mixer and the other is directly injected into the cold main flow. For the first case, the hyper-mixer disperses the injected fuel, leading to the mixing enhancement. Furthermore, the fuel-air mixture is provided into the plasma hot gas, which enhances the combustion performance. However, the direct injection into the main flow method spends amount of fuel without ignition in the cold supersonic flow. In the end, for the forced combustion, it is important to supply the fuel-air mixture into the heat source.

Adaptive Concurrency Control Approach on Shared Object Manipulation in Mixed Reality

  • Lee, Jun;Park, Sung-Jun
    • Journal of the Korea Society of Computer and Information
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    • v.26 no.11
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    • pp.75-84
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    • 2021
  • In this paper, we propose an adaptive concurrency control scheme to reduce conflicts and working time in the cooperative work in mixed reality. To this ends, we first classified the goals, tasks and ownerships of the cooperative work. Then, the classified relationships are mapped according to their temporal and hierarchical relationships of shared object manipulation in the cooperative work. The proposed system provides adaptive concurrency controls of the shared object according to temporal orders of the sub-goals. With the proposed scheme, a participant is enable to move and rotate a shared object although another already has an ownership of the shared object in a specific order of the sub-goal. Thus, the proposed system provides adaptive and realistic cooperative working environment. We conducted a user study of the proposed scheme. The proposed system could reduce conflicts and working times comparing to conventional approaches.

가상제조환경에서 공간상의 충돌검색을 위한 이산사건/연속상태 혼합시뮬레이션

  • 황문호
    • Proceedings of the Korean Society of Machine Tool Engineers Conference
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    • 1999.10a
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    • pp.16-21
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    • 1999
  • 본 연구에서는 컴퓨터 상에 제어기와 구동부 등으로 구성된 가상제조시스템(Virtual Manufacturing System)을 구축하고 시뮬레이션하는 방법론을 다룬다. 특히 설비들간의 이동시 발생할 수 있는 3차원 공간상의 충돌을 검출하는 이산사건 및 연속상태 혼합 시뮬레이션 방법론을 소개한다. 시뮬레이션 모델은 DEVS(discrete event system specification) 형식론(formalsim)에 기초한 형상기구학 정보를 갖는 이른바 GKDEVS(Geometrical Kinematic DEVS)을 이용하였고, 시뮬레이션 방법론은 DEVS의 추상화 시뮬레이션(abstract simulation)방법을 확장하였다.

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Combustion Characteristics of Water Emulsified Fuel by Using Swirl Impinging Mixer (와류 충돌형 혼합장치를 이용한 물혼합 연료의 연소특성)

  • Kwak, I.S.;Han, J.H.;Lee, H.S.;Park, K.
    • Proceedings of the KSME Conference
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    • 2001.06d
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    • pp.852-857
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    • 2001
  • This paper discusses the combustion characteristics of water emulsified fuel produced by swirl impinging mixer. The experiments are given in a test boiler and a commercial boiler. Flame temperatures, flame shapes and exhaust emissions are measured in the test boiler, and thermal efficiency is tested in the commercial boiler. The test data show the water in oil makes the flame wider and shorter, the flame temperature lower and the NOx and smoke lower. Also, the commercial boiler test shows the thermal efficiency increases as well as the emissions decrease.

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Analysis of Spray Combustion for the Performance Prediction of Liquid Rocket Combustor (3차원 분무연소장 해석에 의한 액체추진기관 연소실 성능예측에 대한 연구)

  • 황용석;윤웅섭
    • Journal of the Korean Society of Propulsion Engineers
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    • v.3 no.3
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    • pp.31-39
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    • 1999
  • In this paper, numerical experiment is attempted to analyze and compare the combustion efficiency of the burning sprays due to OFO, FOF triplet / FOOF split doublet injectors. Preconditioned Wavier-Stokes equation system with low Reynolds number $\kappa$-$\varepsilon$ model for turbulence closure, is LU-SGS time-integrated. Spray processes are modeled by DSF analysis with experimentally determined injection characteristics. n-heptane/air global reaction model approximates the combustion for simplicity, and the influence of turbulence on the chemical reaction is included using eddy dissipation model. The results showed the FOF triplet injector of highest combustion efficiency, whereas the OFO type of poet performance. It was also observed that the droplet mean diameter and the average gas temperature due to the mixing efficiency, are the representative parameters for the performance design of combustion.

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Study of Behavior Characteristics of Impinging Spray of Emulsified Fuel (에멀젼연료 충돌분무의 거동특성에 관한 연구)

  • Yeom, Jeong Kuk;Kim, Hak Min
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.39 no.9
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    • pp.909-916
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    • 2015
  • In this study, to investigate the effect of spray behavior characteristics, we induce the mixing ratio of emulsified fuel using impinging spray. We formulate the emulsified fuel by mixing diesel and hydrogen peroxide($H_2O_2$). We set the temperature of the heating plate to $150^{\circ}C$, $200^{\circ}C$, and $250^{\circ}C$, and set the injection pressures to 400, 600, 800, and 1000bar. The surfactants for the emulsified fuel mixture, which were mixed span80 and tween80 was mixed as 9:1, were fixed to 3% of the total volume of the emulsified fuel. We set the mixing ratio of $H_2O_2$ in the emulsified fuel as emulsified fuel(EF)0, EF2, EF12, and EF22. Further, we visualize the evaporation impinging spray using the Schlieren method. Based on the results of this study, we found that a higher temperature and injection pressure of the heating plate impingement led to the active diffusion of the fuel vapor, which promoted emulsified fuel evaporation. When the emulsified fuel is utilized in an actual engine, because of the temperature-drop effect of the combustion chamber, which is due to the evaporation of $H_2O_2$ in fuel and faster mixture formation is expected to decrease the engine emissions.

An Experimental Study on the Characteristics of Spray Pattern and the Mixing Performance of Unlike-impinging Split Triplet Injector(F-O-O-F) (F-O-O-F 충돌형 injector의 분무특성 및 혼합성능에 관한 실험적 연구)

  • Lee, K.J.;Moon, D.Y.;Kim, Y.
    • Journal of the Korean Society of Propulsion Engineers
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    • v.3 no.3
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    • pp.1-8
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    • 1999
  • Mixing efficiency of the unlike Impinging split triplet injector(FOOF type) were measured to investigate the effect of the momentum ratio variation. $H_2$O/kerosene were used as a propellant simulant. The maximum mixing efficiency occured at the momentum ratio 1.5 (total mixture ratio 1.89). Calculated mixing efficiency of real propellant LOX/Kerosene showed similar trend but maximum efficiency of characteristic velocity occurs at the momentum ratio 2.0(total mixture ratio 2.17). Although there exist a little discrepancy between calculated mixing efficiency based on simulant cold test and hot fire test results, this calculated mixing efficiency can be used to predict hot fire mixing efficiency.

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An Experimental Study on Heat Transfer Characteristics of Synthetic Gas($H_2/CO$)Air Premixed Flames in an Impinging Jet Burner - Part 1 : Stretched Lift-off Flames (충돌제트 버너에서 합성가스($H_2/CO$) 공기 예혼합 화염의 열전달 특성에 관한 실험적 연구 - Part 1 : 스트레치된 부상 화염)

  • Kang, Ki-Joong;Jo, Joon-Ik;Lee, Kee-Man
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.04a
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    • pp.453-456
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    • 2011
  • An experimental investigation of the heat transfer characteristics of stretched premixed flames using Synthetic gas has been performed. Hydrogen and carbon mon-oxide which could be extracted from coal gasification process are the main fuel of synthetic-gas. Heat flux at the stagnation point was increased as global strainrate was increased, then the heat flux was decreased when a global strainrate reached a sudden point. Heat flux at the stagnation point is also affected by nozzle to impingement distance. Heat flux was increased as nozzle to impingement place distance was increased. This study is a foundation study of practical use of secondary gases from coals.

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