• 제목/요약/키워드: primary flow

검색결과 1,104건 처리시간 0.047초

아음속/초음속 증기 이젝터에 관한 실험적 연구 (An Experimental Study of the Subsonic/Supersonic Steam Ejectors)

  • 김희동;최보규;이준희
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 추계학술대회논문집B
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    • pp.479-484
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    • 2000
  • For the purpose of a cost effective design of practical subsonic/supersonic ejector systems, an experiment was carried out using a superheated steam as a primary driving flow. The superheated steam jet was produced by several different kinds of subsonic and supersonic nozzles. The secondary flow of atmospheric air inside a plenum chamber was drawn into the primary steam jet. The vacuum performance of the plenum chamber was investigated for a wide range of the ejector operation pressure ratio. The result showed that the static pressure of the mixed flow at the ejector throat is only a function of the ejector operation pressure ratio, regardless of the primary nezzle type employed.

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사행수로의 흐름구조 및 난류특성 (Flow Structure and Turbulence Characteristics in Meandering Channel)

  • 서일원;이규환;백경오
    • 대한토목학회논문집
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    • 제26권5B호
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    • pp.469-479
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    • 2006
  • 본 연구에서는 사행수로에서 주 흐름과 이차류의 특성을 정량적으로 분석하고자 중심각이 $150^{\circ}$이고 사행도 1.52인 S자형 사행수로에서 실험을 수행하였다. 평균수심과 유량을 달리하여 다양한 실험 조건 하에서 수행한 실험을 통해 다중 만곡부를 갖는 사행수로에서 이차류의 공간적 변화양상을 관찰하였다. 실험결과, 주 흐름은 실험조건에 관계없이 직선구간에서 좌우 대칭적인 유속분포를 보였고, 만곡부에서는 내안쪽에 최대유속이 발생하고 외안쪽에 최소유속이 발생하는 현상을 발견 할 수 있었다. 이렇게 주 흐름이 최단노선을 따라 발생하는 현상은 기존 연구자들의 결과와 일치하는 것이다. 이차류의 거동은 첫번째 만곡부보다 두 번째 만곡부에서 더욱 활발하게 발달하고 외안 회전류가 뚜렷히 나타남을 발견하였다. 이차류의 강도는 직선구간에서는 낮게 나타나고 만곡부에서는 증가하는 주기적인 현상을 보였으며, 만곡부의 이차류 강도가 직선구간보다 2~3배 크게 나타났다. 또한, 두 번째 만곡부에서 이차류 강도의 최대값이 발생했다. 주 흐름방향의 난류 강도와 Reynolds 전단응력을 분석한 결과, 주 흐름 난류 강도는 주 흐름의 유속편차가 클수록 증가하는 것으로 나타났고 Reynolds 전단응력은 주 흐름방향 유속의 편차가 크게 벌어지는 동시에 이차류가 활발히 생성되는 지점에서 크게 나타나는 경향을 보였다.

두 대의 펌프가 병렬로 설치된 장치의 유량 특성 (FLOW CHARACTERISTICS OF A SYSTEM WHICH HAS TWO PARALLEL PUMPS)

  • 박정근;박종호;박용철
    • 한국전산유체공학회지
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    • 제17권4호
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    • pp.1-8
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    • 2012
  • During a reactor normal operation, two parallel 50% capacity cooling pumps circulate primary coolant to remove the fission reaction heat of the reactor through heat exchangers cold by a cooling tower. When one pump is failure, the other pump shall continuously circulate the coolant to remove the residual heat generated by the fuels loaded in the reactor after reactor shutdown. It is necessary to estimate how much flow rate will be supplied to remove the residual heat. We carried out a flow network analysis for the parallel primary pumps based on the piping network of the primary cooling system in HANARO. As result, it is estimated that the flow rate of one pump increased about 1.33 times the rated flow of one pump and was maintained within the limit of the cavitation critical flow.

5MW 연구용 원자로의 1차 냉각 계통 유동 특성 (Flow Characteristics of a Primary Cooling System in 5 MW Research Reactor)

  • 박용철;이용섭
    • 한국유체기계학회 논문집
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    • 제13권5호
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    • pp.5-10
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    • 2010
  • 5MW, open pool type research reactor, is commonly used to education and experimental purpose. It is necessary to prepare a standardization of system designs for considering a demand. HANARO has prepared the standardization of 5MW research reactor system designs based on the design, installation, commissioning and operating experiences of HANARO. For maintaining an open pool type reactor safety, a primary cooling system (after below, PCS) should remove the heat generated by the reactor under a reactor normal operation condition and a reactor shutdown condition. For removing the heat generated by the reactor, the PCS should maintain a required coolant flow rate. For a verification of the required flow rate, a flow network analysis of the PCS was carried under a normal operating condition. Based on the flow network analysis result, this paper describes the PCS flow characteristics of a 5MW open pool type research reactor. Through the result, it was confirmed that the PCS met design requirements including design flow rate without cavitation.

Reynolds 수에 따른 꺾어진 덕트에서 열/물질전달 특성 고찰 (Effects of Reynolds Number on Flow and Heat/Mass Characteristics Inside the Wavy Duct)

  • 장인혁;황상동;조형희
    • 설비공학논문집
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    • 제15권10호
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    • pp.809-820
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    • 2003
  • The present study investigates effects of flow velocity on the convective heat/mass transfer characteristics in wavy ducts of a primary surface heat exchanger application. Local heat/mass transfer coefficients on the wavy duct sidewall are determined by using a naphthalene sublimation technique. The flow visualization technique is used to understand the overall flow structures inside the duct. The aspect ratio and corrugation angle of the wavy duct is fixed at 7.3 and 145$^{\circ}$ respectively, and the Reynolds numbers, based on the duct hydraulic diameter, vary from 100 to 5,000. The results show that there exist complex secondary flows and transfer processes resulting in non-uniform distributions of the heat/mass transfer coefficients on the duct side walls. At low Re (Re<1000), relatively high heat/mass transfer regions like cell shape appear on both pressure and suction side wall due to the secondary vortex flows called Taylor-Gortler vortices perpendicular to the main flow direction. However, at high Re (Re>1000), these secondary flow cells disappear and boundary layer type flow characteristics are observed on pressure side wall and high heat/mass transfer region by the flow reattachment appears on the suction side wall. The average heat/mass transfer coefficients are higher than those of the smooth circular duct due to the secondary flows inside wavy duct. And also friction factors are about two times greater than those of the smooth circular duct.

Characteristics of Vortex Structure and Its Shear Velocity in a Scour Hole

  • 김진홍
    • 한국농공학회지
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    • 제34권E호
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    • pp.45-59
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    • 1992
  • At downstream part of the hydraulic structures such as spiliway or drainage gate, jet flow can occur by gate opening. If stream bed is not hard or bed protection is not sufficient, scour hole will be formed due to high shear stress of the jet flow. We call this primary scour. Once the scour hole is formed, a vortex occurs in it and this vortex causes additional scour. We call this secondary scour. The primary scour proceeds to downstream together with flow direction but the secondary one proceeds to upstream direction opposite to it. If the secondary one continues and reaches to the hydraulic structure, it can undermine the bottom of hydraulic structure and this will lead to failure of structure itself. Thus, it is necessary to know the physical features of the vortex structure in a scour hole, which is the main mechanism of the secondary scour. This study deals with the characteristics of the vortex structure and its shear stress which causes the secondary scour.

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두 대의 펌프가 병렬로 설치되는 계통에서의 유량 특성 (Flow Rate Characteristics of Two Parallel Pumping System)

  • 박용철;지대영;서경우;윤현기;박정근
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2011년 춘계학술대회논문집
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    • pp.579-586
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    • 2011
  • During a reactor normal operation, a primary coolant was designed to remove the fission reaction heat of the reactor. When one pump is failure and the other pump shall supply the cooling water to cool the reduced power, it is necessary to estimate how much flow will be supplied to cool the reactor. We carried a flow net work analysis for two parallel pumping system as based on the piping net work of the primary cooling system in HANARO. As result, it is estimated that the flow of one pump increased than the rated flow of the pump below the cavitation critical flow.

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The Effect of the Secondary Annular Stream on Supersonic Jet

  • Lee, Kwon-Hee;Toshiaki Setoguchi;Shigeru Matsuo;Kim, Hyeu-Dong
    • Journal of Mechanical Science and Technology
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    • 제17권11호
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    • pp.1793-1800
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    • 2003
  • The present study addresses an experimental investigation of the near field flow structures of supersonic, dual, coaxial, free, jet, which is discharged from the coaxial annular nozzle. The secondary stream is made from the annular nozzle of a design Mach number of 1.0 and the primary inner stream from a convergent-divergent nozzle. The objective of the present study is to investigate the interactions between the secondary stream and inner supersonic jets. The resulting flow fields are quantified by pitot impact and static pressure measurements and are visualized by using a shadowgraph optical method. The pressure ratios of the primary jet are varied to obtain over-expanded flows and moderately under-expanded flows at the exit of the coaxial nozzle. The pressure ratio of the secondary annular stream is varied between 1.0 and 4.0. The results show that the secondary annular stream significantly changes the Mach disc diameter and location, and the impact pressure distributions. The effects of the secondary annular stream on the primary supersonic jet flow are strongly dependent on whether the primary jet is under-expanded or over-expanded at the exit of the coaxial nozzle.

이차목을 갖는 초음속 이젝터 작동압력에 대한 연구 (Study of Starting Pressure of a Supersonic Ejector with a Second-Throat)

  • 진정근;권세진;김세훈
    • 대한기계학회논문집B
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    • 제29권8호
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    • pp.934-939
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    • 2005
  • Starting pressure of a supersonic ejector with a second-throat was investigated. In case of mixing chamber length longer than a critical length, starting pressure is in proportion to length of the mixing chamber. In this study, we assumed that the ejector starts when the primary supersonic flow reaches inlet of the second-throat and the distance of the supersonic flow traveling can be expressed by multiplying an empirical factor to the first diamond shock length of overexpanded flow. To calculate the overexpanded supersonic flow, a mixing model was employed to compute secondary flow pressure and the result was applied to back pressure condition of overexpanded flow calculation. In the result, for three cases of primary nozzle area ratio, we could get accurate model of predicting the starting pressure by selecting a suitable empirical factors around 3.

광섬유 WOW 액상코팅 공정의 코팅액 유동특성 해석연구 (Analysis of Coating Flow Characteristics in Wet-on-Wet Optical Fiber Liquid Coating Process)

  • 김경진;박중윤
    • 반도체디스플레이기술학회지
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    • 제16권4호
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    • pp.91-96
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    • 2017
  • In this computational study of optical fiber manufacturing, WOW (wet-on-wet) double coating process on freshly drawn glass fiber has been numerical modelled and simulated using a simplified geometry of typical optical fiber coating apparatus. The numerical domain includes primary and secondary coating dies along with secondary coating cup and the interface between primary and secondary coating liquids are investigated using level set method. Coating liquid viscosity is an important parameter and its dependence on temperature is also considered. Since there would be possibility for pressure and temperature of primary coating liquid to be increased substantially at high fiber drawing speed, the effects of increased pressure and temperature of primary coating liquid are examined on flow patterns of coating liquids in secondary coating cup. In case that both pressure and temperature of primary coating liquid are high enough, liquid interface becomes noticeably unstable and this flow instability could adversely affect the uniform coatings and final quality of produced optical fiber.

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