• Title/Summary/Keyword: Flow Choke

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A Study on the Choke Phenomenon of Unsteady Gas Flow through a Critical Nozzle (임계노즐을 통한 비정상 기체유동의 초크현상에 관한 연구)

  • Kim, Jae-Hyung;Kim, Heuy-Dong;Park, Kyung-Am
    • Proceedings of the KSME Conference
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    • 2003.04a
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    • pp.2127-2132
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    • 2003
  • A computational study is performed to better understand the choke phenomenon of unsteady gas flow through a critical nozzle. The axisymmetric, unsteady, compressible, Navier-Stokes equations are solved using a finite volume method. In order to simulate the effects of back pressure fluctuations on the critical nozzle flow, a forced sinusoidal pressure wave is assumed downstream the exit of the critical nozzle. It's frequency is 20kHz and amplitude is varied below 15% of time-mean back pressure. The results obtained show that for low Reynolds numbers, the unsteady effects of the pressure fluctuations can propagate upstream of the throat of critical nozzle, and thereby giving rise to applicable fluctuations of mass flow through the critical nozzle. The effect of the amplitude of the excited pressure fluctuations on the choke phenomenon is discussed in details.

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Rotating Choke and Choked Surge in an Axial Pump Impeller

  • Watanabe, Toshifumi;Sato, Hideyoshi;Henmi, Yasuhiko;Horiguchi, Hironori;Kawata, Yutaka;Tsujimoto, Yoshinobu
    • International Journal of Fluid Machinery and Systems
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    • v.2 no.3
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    • pp.232-238
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    • 2009
  • Unlike usual turbopump inducers, the axial flow pump tested operates very stably at design flow rate without rotating cavitation nor cavitation surge. Flow visualization suggests that this is because the tip cavity smoothly extends into the flow passage without the interaction with the leading edge of the next blade. However, at low flow rate and low cavitation number, choked surge and rotating choke were observed. Their correlation with the performance curve under cavitation is discussed and their instantaneous flow fields are shown.

Air Influx Characteristics of Turbo Pumps (공기 유입시의 터보펌프 특성)

  • Kim, You-Taek;Nam, Cheong-Do;Kang, Ho-Keun;Lee, Young-Ho
    • 유체기계공업학회:학술대회논문집
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    • 2004.12a
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    • pp.43-48
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    • 2004
  • A screw-type centrifugal pump was manufactured to carry solids primarily and its impeller has a wide flow passage. However, the effect of flow passage shape on delay of the choke due to entrained air has not been clarified yet. Moreover, because its impeller has a particular shape, only few studies have tried to clarify the pump performance and details of internal flow pattern of that pump. For that reason, we carried out the pump performance experiment under air-water two-phase flow condition with different impeller tip clearances, pump rotational speeds and void fractions by using a small screw-type centrifugal pump designed to acquire basic data. In a general centrifugal pump, it was reported that loss of pump head from single-phase flow to the choke due to air entrainment new the best efficiency point was large. However, the loss near the best efficient point in a screw-type centrifugal pump became less than that in a general centrifugal pump.

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Frequency Characteristics of Unsteady Flow of Cylindrical Choke in a Hydraulic Pipe (유압관로에서 원통형 초크의 비정상 유동의 주파수 특성에 관한 연구)

  • Park, S.J.;Yoo, Y.T.;Wee, K.H.
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.7 no.3
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    • pp.421-434
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    • 1995
  • A new instantaneous flowmeter for hydraulics by means or cylindrical chokes is developed. In this method the instantaneous flowrate through chokes is predicted in real time from measurement of pressure difference on both sides of cylindrical choke. The experimental study for the flowrate of pulsating flow in a pipe is carried out to measure differential pressure drop by using a strain gauge pressure transducer with data acquisition and processing system. A pulsating flow is verified by a visualization method. In the present study, the flow characteristic variables of laminar pulsating flow are investigated analytically and experimentally in a circular pipe. Characteristic parameters of ratio of inertia term to pressure term($\phi_{t.1}$) and ratio of viscous term to pressure term($\phi_{z.1}$) are introduced to describe the flow pattern of laminar pulsating flow.

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A Study on Pressure Distributions in a Centrifugal Compressor Channel Diffuser (원심압축기 채널디퓨저 내부의 압력분포에 관한 연구)

  • Gang, Jeong-Sik;Gang, Sin-Hyeong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.25 no.4
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    • pp.507-513
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    • 2001
  • Time averaged pressure distributions in a high-speed centrifugal compressor channel diffuser at design and off-design flow rates are investigated. Pressure distributions from the impeller exit to the channel diffuser exit are measured for various flow rates from choke to near surge condition, and the effects of operating condition are discussed. The strong non-uniformity in the pressure distribution is obtained over the vaneless space and semi-vaneless space caused by the impeller-diffuser interaction. As the flow rate increases, flow separation near the throat, due to large incidence angle at the vane leading edge, increases aerodynamic blockage and reduces the aerodynamic flow area downstream. Thus the minimum pressure location occurs downstream of the geometric throat, and it is named as the aerodynamic throat. And at choke condition, normal shock occurs downstream of this aerodynamic throat. The variation in the location of the aerodynamic throat is discussed.

A Study on the Pressure Distribution in the Centrifugal Compressor Channel Diffuser at Design and Off-Design Conditions (설계 및 탈설계점에서의 원심압축기 채널디퓨저 내부의 압력분포에 관한 연구)

  • Kang, Jeong-Seek;Kang, Shin-Hyoung
    • Proceedings of the KSME Conference
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    • 2000.04b
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    • pp.548-554
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    • 2000
  • The aim of this paper is to understand the time averaged pressure distributions in a high-speed centrifugal compressor channel diffuser at design and off-design flow rates. Pressure distributions from the impeller exit to the channel diffuser exit are measured and discussed far various flow rates from choke to near surge condition, and the effect of operating condition is discussed. The strong non-uniformity in the pressure distribution is obtained over the vaneless space and semi-vaneless space caused by the impeller-diffuser interaction. As the flow rate increases, flow separation near the throat, due to large incidence angle at the vane leading edge, increases aerodynamic blockage and reduces the aerodynamic flow area downstream. Thus the minimum pressure location occurs downstream of the geometric throat, and it is named as the aerodynamic throat. And at choke condition, normal shock occurs downstream of this aerodynamic throat. The variation in the location of the aerodynamic throat is discussed.

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Characteristics of a Small Screw-type Centrifugal Pump Operating in Air-Water Two-Phase Flow (소형 스크류식 원심펌프의 기액 이상류 특성)

  • Kim, You-Taek;Tanaka, Kazuhiro;Lee, Young-Ho
    • The KSFM Journal of Fluid Machinery
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    • v.2 no.4 s.5
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    • pp.9-15
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    • 1999
  • A screw-type centrifugal pump was manufactured to carry primarily solids and its impeller had a wide flow passage. However, there was an effect on the flow passage shape on delay of the choke due to entrained air not being clarified yet. Moreover, because its impeller has a particular shape, only few studies have tried to clarify the pump performance and details of internal flow pattern of that pump. For this reason, we carried out the pump performance experiment under air-water two-phase flow condition with different impeller tip clearances, pump rotational speeds and void fractions by using a small screw-type centrifugal pump designed to acquire basic data. In a general centrifugal pump, it was reported that there was a loss of pump head from single-phase flow to the choke due to air entrainment near the best efficiency point being large. However, the loss near the best efficient point in a screw-type centrifugal pump became less than that in a general centrifugal pump.

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An Analytical Study for Critical Mass Flowrate of Compressed Water (압축수의 임계유량에 관한 해석적 연구)

  • 김희동;김재형;한민교;박경암
    • Journal of the Korean Society of Propulsion Engineers
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    • v.7 no.1
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    • pp.57-65
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    • 2003
  • As a compressed water is rapidly expanded through a nozzle, two-phase flow of vapor and liquid is formed in the nozzle due to the flash evaporation. In the present study, critical flow of two-phase fluids is analysized using an Isentropic-Homogeneous-Equilibrium model and a Leung model. Calculation results show that the choke of the two-phase flow can be two different types of continuous and discontinuous chokings. For the stagnation pressure below 10 Mpa it is found that the continuous choking, which is similar to the choking phenomenon of single-phase gas flow, is possible only when the degree of subcooling is less than 10K.

Behaviour of Pulsating Flow in the Jetflow Region through Cylindrical Chokes (원통형 초크의 분류영역에서 맥동유동의 거동)

  • Moh, Y.W.;Yoo, Y.T.;Hong, S.S.;Wee, K.H.
    • Transactions of the Korean Society of Automotive Engineers
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    • v.3 no.5
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    • pp.47-55
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    • 1995
  • Cylindrical chokes are used widely as components of hydraulic equipments. The dynamic charac teristics between flowrate and pressure drop through the cylindrical chokes were discussed by the frequency characteristics of the chokes. It was assumed no pressure recovery occured at the downstream neighborhood of the choke. The pulsating jetflow from outlet of cylindrical chokes shows very complex behaviours which are quite different from the steady jetflow but it is not clarified quantitatively. In order to utilize the chokes as a flowmeter, it is indispensable to discuss the estimation of the dynamics of pressure drop in the downstream jetflow region of cylindrical chokes. In this experimental study, the dynamic behaviours of the jetflow in the downstream region of cylindrical chokes are investigated precisely by using flow visualization. In the results of experimental sutdy, it is clarified that the retachment length depended on pressure wave is compared with it depended on velocity wave.

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A Numerical Study on Aerodynamic Performance by the Blade Mach Number of the Centrifugal Compressor (원심 압축기의 임펠러 마하수에 따른 공력성능 특성에 관한 수치해석적 연구)

  • Heo, Won-Seok;Kang, Shin-Hyoung
    • The KSFM Journal of Fluid Machinery
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    • v.18 no.4
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    • pp.56-61
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    • 2015
  • It is important requirement to properly evaluate the aerodynamic performance and characteristics during preliminary design of a centrifugal compressor. In this study the centrifugal compressor was calculated for variations of mass flow and blade Mach number by means of single passage steady state. A lot of quantitative performance values were obtained and through the obtained values the aerodynamic performance characteristics of designed impeller and vaned diffuser were investigated. The results were classified by blade Mach number to analyze characteristics and the aerodynamic performance was examined at choke of impeller, diffuser and separation of diffuser.