• 제목/요약/키워드: Dual Flow

검색결과 515건 처리시간 0.027초

수평 원주형 환형내에서의 정상상태의 공기의 자연대류에 대한 이중해 (Dual Solutions for Steady Natural Convection of Air in Horizontal Cylindrical Annulus)

  • 유주식
    • 대한기계학회논문집B
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    • 제20권9호
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    • pp.2981-2990
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    • 1996
  • Dual solutions for steady natural convection of air between two horizontal concentric cylinders are numerically investigated in the range of $D_i$/TEX>/L(=diameter of inner cylinder/gap width)$\leq$10. It is found that, when the Rayleigh number based on the gap width exceeds a certain critical value, a new flow pattern forming two counter-rotating eddies in the half of the annulus can be realized, which is different from the crescent-shaped flow commonly observed. In the new flow pattern, the fluid near the top of the hot inner cylinder moves downward. This solution is found for D$_{i}$/L.geq.0.3, but not for$D_i$/TEX>/L$\leq$0.2. As $D_i$/TEX>/L increase, the critical Rayleigh number is decreased, and tends to a finite limit.t.

지하공간 침수해석모형과 연계한 도시침수해석 통합모형 (Integration Model for Urban Flood Inundation Linked with Underground Space Flood Analysis Model)

  • 이창희;한건연
    • 한국수자원학회논문집
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    • 제40권4호
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    • pp.313-324
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    • 2007
  • 비정형격자 기반의 수치해석모형을 이용하여 지하공간침수해석모형을 개발하였다. 본 모형은 지하공간의 흐름 특성을 link-node 시스템에 의해 해석하고, 계단 및 벽구조물 등의 지하공간 구조물 배치 영향을 고려한 침수해석을 수행할 수 있다. 흐름은 두가지로 구분하며, 하나는 두 개의 인접한 격자가 지하공간에서의 지하철 노선에 해당되어 수로형 흐름을 나타내는 경우이고, 다른 하나는 지하공간에서의 지하철 노선 이외의 지점 및 지하상가 등으로 물이 확산되는 위어형 흐름인 경우이다. ArcGIS 시스템의 Visual Basic Application을 이용하여 Dual-Drainage 침수해석 모형과 지하공간침수해석 모형이 통합하였다. 개발된 통합모형은 홍수관계기관이 침수 발생이 예상되는 지점에서 홍수피해 방지를 위해 배수시스템의 용량에 대한 재설계 흑은 확장 등과 같은 대책을 수립하는데 도움을 줄 수 있고, 침수위험지도작성 및 홍수경감대책을 수립하는데 이용될 수 있다.

물질전달계수를 이용한 생물 반응기 운전 최적화 (Optimization of Bioreactor Operation by Mass Transfer Coefficient)

  • 김형순
    • 한국산업융합학회 논문집
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    • 제4권3호
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    • pp.243-251
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    • 2001
  • The effects of various operating parameters(agitation speed, impeller type, antiform agents, impeller spacing etc.) on air-liquid mass transfer was characterized by volumetric mass transfer coefficient($k_La$). Also, the dual-impeller agitated systems are compared with single-impeller agitated systems with a special focus on its applications for bioreactors, $k_La$ was take over a range of 200~450 rpm of agitation speed, and 0.5~2.5 vvm of air flow rates, for four single impeller and impeller combinations consisting of four impeller types, namely rushton, pitched blade, scaba, intermig were tested. The rushton impeller showed the best $k_La$ as compared with other single impellers. The dual impeller system are found to be superior as compared to single impeller in all aspects, The best combination of the dual impeller was a intermig of axial flow type as an upper impeller and a rushton of radial flow type as a lower part. Also, the control of the DO level with the variation of agitation speed was more efficient than that with an increase in air flow rate. The addition of antiform dropped the $k_La$ very large up to 1g/L regardless the type. PPG was less effect on $k_La$ than other antiforms. The impeller spacing and presence of solute are found very effective on $k_La$. When the $NaNO_3$is presented as solute, the $k_La$ increased approximately 50% then control.

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마이크로 가스터빈을 위한 하이브리드/이중 선회제트 연소기의 개발 (Part I: 형상 최적화를 위한 실험적 연구) (Development of a Hybrid/Dual Swirl Jet Combustor for a Micro-Gas Turbine (Part I: Experimental Study on Geometric Optimization))

  • 박태준;황철홍;이기만
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2012년도 제44회 KOSCO SYMPOSIUM 초록집
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    • pp.199-200
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    • 2012
  • An experimental study on geometric optimization was conducted to develop a hybrid/dual swirl jet combustor for a micro-gas turbine. A hybrid concept indicating a combination of swirling jet partially premixed and premixed flames were adopted to achieve high flame stability as well as clean combustion. Location of pilot nozzle, angle and direction of swirl vane were varied as main parameters with a constant fuel flow rate for each nozzle. The results showed that the variation in location of pilot nozzle resulted in significant change in swirl intensity due to the change in flow area near burner exit, and thus, optimized nozzle location was determined on the basis of CO and NOx emissions under conditions of co-swirl flow and swirl $angle=30^{\circ}$. The increase in swirl angle (from $30^{\circ}$ to $45^{\circ}$) enhanced the emission performances, in particular, with a significant reduction of CO emission near lean-flammability limit. It was observed that the CO emission near lean-flammability limit was further reduced through the counter-swirl flow. However, there was not significant change in the NOx emission in the operating conditions (i.e. equivalence ratio of 0.6~0.7) between the co- and the counter-swirl flow.

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2중스월류에 의한 난류분무화염의 연소특성 연구 (A Study on Combustion Characteristics of Turbulent Spray Flame by the Dual Swirler)

  • 이강엽;황상순
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2000년도 제20회 KOSCO SYMPOSIUM 논문집
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    • pp.105-116
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    • 2000
  • An Experimental study was conducted on spray combustion using dual swirlers at different outlet angle; co-swirl and counter-swirl. To understand the characteristics of turbulent spray combustion of dual swril flow(DSF), the axial helical annular vaned swirlers with various swirl ratios and combination of angle and direction were designed. and temperature measurements of a rapidly thermocouple insertion and measurements of soot volume fraction and microrstructure using thermophoretic sampling particle diagnostic(TSPD) as TEM were carried out. The NOx, $CO_2$,$O_2$, etc. was analyzed using emission gas analyzer. The results show that flame stability were maintained under very lean condition. for both co-swirl and counter-swirl case. And though Counter-swirl case kept the higher temperature region compared to co-swirl case, Counter-swirl combustion represented less NOx emission and soot formation than co-swirl case.

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2중스월류에 의한 난류분무화염의 연소특성 연구 (A Study on Combustion Characteristics of Turbulent Spray Flame by the Dual Swirler)

  • 이강엽;황상순
    • 한국연소학회지
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    • 제5권1호
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    • pp.67-79
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    • 2000
  • An Experimental study was conducted on spray combustion using dual swirlers at different outlet angle; co-swirl and counter-swirl. To understand the characteristics of turbulent spray combustion of dual swril flow(DSF), the axial helical annular vaned swirlers with various swirl ratios and combination of angle and direction were designed. and temperature measurements of a rapidly thermocouple insertion and measurements of soot volume fraction and microstructure using thermophoretic sampling particle diagnostic(TSPD) as TEM were carried out. The NOx, $CO_2,\;O_2$, etc. was analyzed using emission gas analyzer. The results show that flame stability were maintained under very lean condition. for both co-swirl and counter-swirl case. And though Counter-swirl case kept the higher temperature region compared to co-swirl case, Counter-swirl combustion represented less NOx emission and soot formation than co-swirl case.

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PIV를 이용한 이중 충돌제트의 유동 특성 (Flow Characteristics of Dual Impinging Jets using PIV)

  • 김동건;권순홍;정성원;박종민;최원식;김종순;권순구
    • 한국기계가공학회지
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    • 제10권6호
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    • pp.102-108
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    • 2011
  • The flow characteristics of unventilated dual impinging jets were experimentally investigated. Two nozzles with an aspect ratio of 20 were separated by 6 nozzle widths. The Reynolds number based on nozzle width and nozzle exit velocity was set to 5,000. A Particle Image Velocimetry (PIV) was used to measure turbulent velocity components. It was found that, when an impingement plate was installed in the converging region, there was a stagnation region in the inner area between nozzles. However, when it was installed in the combined region, both jets were merged and collided into the plate, showing single-jet characteristics. In addition, at a dual impinging jet, as the distance between a nozzle and an impingement plate decreased, the spanwise turbulent intensity at the plate increased.

이중구조 오리피스 팽창장치의 유동특성에 관한 실험적 연구 (An Experimental Study on Flow Characteristics for Dual-Structured Orifice)

  • 곽경민;김하덕;이중형;배철호;김종엽
    • 설비공학논문집
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    • 제14권12호
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    • pp.1039-1046
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    • 2002
  • To investigate the characteristics of orifice as an expansion devices, the experimental apparatus was made and experiments are being peformed using R22 and R290. The main idea of this control method of refrigerant flow rate with coupled orifices is to control the ON/OFF state of T and Ball type orifice corresponding to the subdivided region of thermal load. When system requires minimum thermal load, both T and Ball type orifices are closed, but refrigerant can flow through small hole of T type orifice. In regular thermal load, when ball type orifice is closed, T type orifice is opened and mass flow rate increase more than OFF state of T type orifice, due to large diameter. In maximum thermal load, both T and Ball type orifices are open and the much refrigerant can flow. The flow characteristics on T type orifice and parallel-combined orifice are obtained in the subdivided region of thermal load.

Electrodeposition of GMR Ni/Cu Multilayers in a Recirculating Electrochemical Flow Reactor

  • Rheem, Young-Woo
    • 한국재료학회지
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    • 제20권2호
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    • pp.90-96
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    • 2010
  • The recirculating electrochemical flow reactor developed at UCLA has been employed to fabricate nanostructured GMR multilayers. For comparison, Ni/Cu multilayers have been electrodeposited from a single bath, from dual baths and from the recirculating electrochemical flow reactor. For a magnetic field of 1.5 kOe, higher GMR (Max. -5%) Ni/Cu multilayers with low electrical resistivity (< $10\;{\mu}{\Omega}{\cdot}cm$) were achieved by the electrochemical flow reactor system than by the dual bath (Max. GMR = -4.2% and < $20\;{\mu}{\Omega}{\cdot}cm$) or the single bath (Max. GMR = -2.1% and < $90\;{\mu}{\Omega}{\cdot}cm$) techniques. Higher GMR effects have been obtained by producing smoother, contiguous layers at lower current densities and by the elimination of oxide film formation by conducting deposition under an inert gas environment. Our preliminary GMR measurements of Ni/Cu multilayers from the electrochemical flow reactor obtained at low magnetic field of 0.15 T, which may approach or exceed the highest reported results (-7% GMR) at magnetic fields > 5 kOe.