• 제목/요약/키워드: Equilibrium Air

검색결과 301건 처리시간 0.028초

R-134a/PAG 오일 혼합물의 용해도 및 상용성 측정 (Measurement of solubility and miscibility of R-134a/PAG oil mixture)

  • 김창년;송준석;박영무
    • 설비공학논문집
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    • 제11권4호
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    • pp.518-527
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    • 1999
  • The solubility and miscibility measurement apparatus has been developed and used to obtain data for refrigerant/oil mixture. The solubility and miscibility data for R-134a/46 ISO VG Polyalkylen Glycol(PAG) oil mixture are obtained over the temperature range from -20 to 6$0^{\circ}C$ with a 1$0^{\circ}C$ interval and the oil concentration range from 0 to 90wt%. Using the experimental data, an empirical model is developed to predict the solubility relations for R-134a/PAG oil mixture at equilibrium. The average root-mean-square deviation between measured data and calculated results from the empirical model is 4.2%. Raoult's rule and Flory-Noggins theory are also used to predict mixture behavior. Immiscibility is observed for R-134a/46 ISO VG PAG oil mixture at low oil concentrations of 4.6, 10.1, and 20.4wt%.

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탄화수소 및 불화탄화수소 혼합냉매의 기상-액상 평형에 관한 실험적 연구 (An Experimental Study on Vapor-Liquid Equilibria of HFC and HC Refrigerant Mixtures)

  • 강병복;김민수;김영일
    • 설비공학논문집
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    • 제12권11호
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    • pp.1031-1037
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    • 2000
  • Isothermal vapor-liquid equilibrium(VLE) data have been obtained for the systems of propane(R290)+1,1,1,2-tetrafluoroethane(R134a) and 1,1,1,2-tetrafluoroethane(R134a)+isobutane(R60A) in the temperature range of 253.15 to 323.15K. Experiments were performed in a circulation type apparatus by injecting vapor through liquid pool using a magnetic pump. Both systems form azeotropes in the temperature range of this study. The experimental results were estimated with the Peng-Robinson equation of state. When the temperature-dependent binary interaction parameter was used in the Peng-Robinson equation of state, the absolute average deviation of the measured bubble point pressures from the values correlated by the Peng-Robinson equation was 0.65% and 0.78% for R290+R134a and R134a+600a, respectively. Azeotropic compositions for both systems were presented.

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가옥 및 실험실내 라돈평형인자, 비 흡착 라돈자손 비율의 일일 변동 특성 (Diurnal Variations of Equilibrium Factor and Unattached fraction of Radon Progeny in Some Houses and Laboratories)

  • 이승찬;김창규;이동명;강희동
    • Journal of Radiation Protection and Research
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    • 제26권4호
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    • pp.399-408
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    • 2001
  • 일반가옥 및 실험실에서 라돈농도, 평형등가농도 및 평형인자의 농도 변화를 검토하였으며, 환기조건에 따른 평형인자, 비흡착 라돈자손 비율의 변통 특성을 검토하였다. 가옥 7개 지점에서의 평균 라돈농도, 평형등가농도 및 평형인자는 각각 $30\;Bq\;m^{-3},\;19.6\;Bq\;m^{-3}$, 0.65였다. 한편, 실험실 3개 지점에서의 평균 라돈농도, 평형등가농도 및 평형인자는 각각 $55.0\;Bq\;m^{-3},\;31.9\;Bq\;m^{-3}$, 0.58였다 실내에서의 라돈농도, 평형등가농도 및 평형인자는 새벽 및 아침시간에 높고 오후 4시부터 밤 10시 사이에 낮아지는 주기적인 특성을 나타내었다 환기상태가 좋은 경우가 환기상태가 나쁜 경우에 비해 평형인자는 낮아지는 반면, 비 흡착 라돈자손 비율이 증가하는 경향을 나타내었으며, 평형인자는 기압, 습도에 비례하는 반면, 온도에는 반비례하는 관계를 나타내었다.

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고온 열기 처리에 의한 낙엽송재의 물리·역학적 성능 및 내부후성능 변화 고찰 (Evaluation of Physico-Mechanical Properties and Durability of Larix kaempferi Wood Heat-Treated by Hot Air)

  • 박용건;한연중;박준호;장윤성;양상윤;정현우;김경중;여환명
    • Journal of the Korean Wood Science and Technology
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    • 제43권3호
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    • pp.334-343
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    • 2015
  • 본 연구에서는 국내에서 상업적으로 이용되고 있는 국산 낙엽송 열처리재의 여러 가지 물성(밀도, 평형함수율, 수축률, 흡습/흡수성, 종/횡압축강도, 휨강도, 경도, 내부후성능)을 정량적으로 평가하기 위하여 수행되었다. 고온처리에 의해 목재의 소수성이 증가함에 따라 평형함수율이 감소하였다. 이에 따라 수축률 및 흡습/흡수성이 감소하여 치수안정성이 개선되었고, 낮은 함수율의 영향으로 압축강도가 증가하였으며, 목재 주성분의 변화와 낮은 함수율의 영향으로 내부후성능이 개선되었다. 하지만 열처리에 의해 밀도와 휨강도 및 경도는 감소하였다.

충돌 공기제트에서 국한 유로 내 발포 알루미늄 방열기의 열전달 수치해석 (A Numerical Study on Beat Transfer from an Aluminum Foam Heat Sink by Impinging Air Jet in a Confined Channel)

  • 이상태;김서영;이관수
    • 대한기계학회논문집B
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    • 제26권6호
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    • pp.883-892
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    • 2002
  • A numerical study has been carried out to investigate the flow and heat transfer from an aluminum foam heat sink in a confined channel. A uniform heat flux is given at the bottom of the aluminum foam heat sink, which is horizontally placed on the heated surface. The channel walls are assumed to be adiabatic. Cold air is supplied from the top opening of the channel and exhausted to the channel outlet. Comprehensive numerical solutions are acquired to the governing Wavier-Stokes and energy equations, using the Brinkman-Forchheimer extended Darcy model and the local thermal non-equilibrium model f3r the region of porous media. Details of flow and thermal fields are examined over wide ranges of the principal parameters; i.e., the Reynolds number Re, the height of heat sink h/H, porosity $\varepsilon$and pore diameter ratio $R_{H}$.

Simulink를 이용한 고분자 전해질 연료전지 시스템 시뮬레이션 (Polymer Electrolyte Fuel Cell Simulation Using Simulink)

  • 황남선;이호준;주병수
    • 한국신재생에너지학회:학술대회논문집
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    • 한국신재생에너지학회 2007년도 춘계학술대회
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    • pp.109-112
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    • 2007
  • In this paper, a mathematical modeling was developed to simulate 1kW class air cooled Polymer Electrolyte Membrane Fuel Cell(PEMFC) system. The proposed modeling was conducted under SIMULINK based environment. The model ing was developed based on the thermodynamic and chemical equilibrium. The objective is to design and implement the entire fuel cell system model ing including the system controller modeling. The fuel cell process and the control system modeling should have to be connected with each other simultaneously, therefore the two types of modeling influences each other when the system simulator run. The fuel cell modeling libraries are simulated using the SIMULINK under the thermodynamic and chemical equilibrium base. The PID controller application was designed and developed to test the process modeling and verify it. This the prototype development of the fuel cell system to design and test more complicate fuel cell systems, like the residential power generation system. The simulation results was compared to the real PEMFC system performance. We have achieved the reasonable accordance with the Lab test and the simulation results.

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Backhaul transmission scheme for UAV based on improved Nash equilibrium strategy

  • Liu, Lishan;Wu, Duanpo;Jin, Xinyu;Cen, Shuwei;Dong, Fang
    • KSII Transactions on Internet and Information Systems (TIIS)
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    • 제16권8호
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    • pp.2666-2687
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    • 2022
  • As a new alternative communication scheme in 5G, unmanned aerial vehicle (UAV) is used as a relay in the remote base station (BS) for assistant communication. In order to ameliorate the quality of the backhaul link, a UAV backhaul transmission scheme based on improved Nash equilibrium (NE) strategy is proposed. First, the capacity of air-to-ground (A2G) channel by the link preprocess is maximized. Then, the maximum utility function of each UAV is used as the basis of obtaining NE point according to the backhaul channel and the backhaul congestion. Finally, the improved NE strategy is applied in multiple iterations until maximum utility functions of all the UAVs are reached, and the UAVs which are rejected by air-to-air (A2A) link during the process would participate in the source recovery process to construct a multi-hop backhaul network. Simulation results show that average effective backhaul rate, minimum effective backhaul rate increases by 10%, 28.5% respectively in ideal A2G channel, and 11.8%, 42.3% respectively in fading channel, comparing to pure NE strategy. And the average number of iterations is decreased by 5%.

천음속 익형 유동에서 비평형 응축이 Drag Divergence Mach Number에 미치는 영향에 관한 수치 해석적 연구 (Numerical Study on the Effect of Non-Equilibrium Condensation on Drag Divergence Mach Number in a Transonic Moist Air Flow)

  • 최승민;강희보;권영두;권순범
    • 대한기계학회논문집B
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    • 제40권12호
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    • pp.785-792
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    • 2016
  • 본 연구에서는 NACA0012 천음속 익형 유동에 있어 비평형 응축이 항력 발산 마하수 $M_D$에 미치는 영향을 TVD 유한 차분법을 사용하여 연구하였다. 받음각 ${\alpha}$가 동일한 경우, 정체점 상대습도 ${\phi}_0$가 높을수록 충격파 직전의 최대 마하수 $M_{max}$는 작게 되고 초음속 영역의 크기도 적게 된다. 주류 마하수 $M_{\infty}$, 정체점 상대습도 ${\phi}_0$ 및 정체온도 $T_0$가 동일한 경우 받음각 ${\alpha}$가 클수록 비평형 응축영역 길이 ${\Delta}_z$은 짧게 된다. 한편, 주류 마하수 $M_{\infty}$와 받음각 ${\alpha}$가 동일한 경우 정체점 상대습도 ${\phi}_0$가 높을수록 조파저항의 감소 때문에 항력계수 $C_D$는 적어진다. $M_D$${\alpha}$가 동일한 경우 ${\phi}_0$가 클수록 크게 되며, ${\phi}_0$가 동일한 경우는 ${\alpha}$가 클수록 $M_D$는 적게 된다.

3단형 과학로켓 탑재부 극초음속 공력특성 연구 (Numerical Study on Hypersonic Characteristics of the KSR-Ⅲ Payload)

  • 이장연
    • 한국전산유체공학회지
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    • 제6권2호
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    • pp.32-39
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    • 2001
  • Hypersonic analysis on the KSR-Ⅲ payload configuration has been performed using an axisymmetric Navier-Stokes code. A numerical code based on the Harten and Yee's upwind TVD scheme with simplified curve fits in the chemically reacting equilibrium air was developed. The carbuncle phenomenon on detached shock in front of the payload is controlled by using pressure gradients to tune the dissipation. Chemically reacting equilibrium computations for the reentry flight conditions of Mach No. 10.2, 8, 4.9 are presented and compared with the results of calorically perfect gas.

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Finite Volume Analysis of a Supersonic Non-Equilibrium Flow Around an Axisymmetric Blunt Body

  • Haoui, R.
    • International Journal of Aeronautical and Space Sciences
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    • 제11권2호
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    • pp.59-68
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    • 2010
  • The aim of this work is to analyze high temperature flows around an axisymmetric blunt body taking into account chemical and vibrational non-equilibrium state for air mixture species. For this purpose, a finite volume methodology is employed to determine the supersonic flow parameters around the axisymmetric blunt body. This allows the capture of a shock wave before a blunt body placed in supersonic free stream. The numerical technique uses the flux vector splitting method of Van Leer. Here, adequate time stepping parameters, along with Courant, Friedrich, Lewis coefficient and mesh size level are selected to ensure numerical convergence, sought with an order of $10^{-8}$.