• 제목/요약/키워드: Orifice discharge coefficient

검색결과 44건 처리시간 0.026초

Numerical Analysis on the Discharge Characteristics of a Liquid Rocket Engine Injector Orifice

  • Cho, Won-Kook;Kim, Young-Mog
    • International Journal of Aeronautical and Space Sciences
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    • 제3권1호
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    • pp.1-8
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    • 2002
  • A numerical analysis was performed on the fluid flow in injector orifice of a liquid rocket engine. The present computational code was verified against the published data for turbulent flow in a pipe with a sudden expansion-contraction. Considered were the parameters for the flow analysis in an injector orifice: Reynolds number, ratio of mass flow rate of the injector orifice and inlet flow rate, and slant angle of the injector orifice. The discharge coefficient increased slightly as the Reynolds number increased. The slant angle of the injector changed critically the discharge coefficient. The discharge coefficient increased by 7% when the slant angle changed from $-30^{\circ}$ to $30^{\circ}$ The ratio of mass flow rate had relatively little impact on the discharge coefficient.

오리피스 전단에 인접한 $90^{\circ}$엘보와 오리피스간의 거리가 유출계수에 미치는 영향 (The Effect of Distance between $90^{\circ}$Elbow close to Upstream Face of Orifice Plate and Orifice Plate on Discharge Coefficient)

  • 윤준용;성낙원
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.357-360
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    • 2002
  • The effect of distance between ninety degree elbow close to upstream face of orifice plate and orifice plate on discharge coefficient was investigated. The distributions of discharge coefficient and differential pressure caused by elbow and short upstream straight length were examined and modified discharge coefficient was introduced. The results presented in this study could be useful when orifice plate is installed under the condition of simple flow disturbance element and short upstream straight length.

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전산유동해석을 이용한 ORIFICE 방출 계수 예측 (PREDICTION OF THE ORIFICE DISCHARGE COEFFICIENT USING COMPUTATIONAL FLUIDS DYNAMICS)

  • 옥호남;김인선
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2006년도 추계 학술대회논문집
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    • pp.147-150
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    • 2006
  • Vent ports are installed on the walls of closed compartments of a launch vehicle to control the pressure drop in the compartments. The ports can be modelled as an orifice, and the accurate prediction of the discharge coefficient of an orifice is essential for the design of vent ports. Experimental methods have been used to determine the discharge coefficients for various shapes of orifices, and extensive databases are available. Wind tunnel tests have been also done to evaluate the effect of interaction between venting outflow and freestream for limited conditions. The goal of the present research is to predict the discharge coefficient of an orifice using CFD and evaluate the accuracy of the method, especially for the orifices exposed to the external flow.

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오리피스를 통하는 임계 기체 유동에 관한 연구 (Study of the Critical Gas Flow through an Orifice)

  • 김재형;김희동;박경암
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 추계학술대회
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    • pp.532-537
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    • 2003
  • Gas flow through orifice is encountered in many diverse fields of engineering applications. In order to investigate the critical gas flow through an orifice system, a computational analysis is performed using axisymmetric, compressible, Navier-Stokes equations which are numerically solved by a fully implicit finite volume method. In the present study, the discharge coefficients of two different types of orifices which are a straight-bore orifice and a sharp-edged orifice, are predicted to obtain the critical flow conditions. The present CFD data are compared with the previous experimental results. The present computational results show that the critical mass flow rate through orifice is well predicted and it is a strong function of Reynolds number. The discharge coefficient increases with the orifice diameter.

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차압식 유량계에서 점탄성유체의 유출 및 손실계수 (Discharge and loss coefficients for viscoelastic fluids in differential pressure flow meters)

  • 전우청;조병수;백병준;박복춘
    • 대한기계학회논문집B
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    • 제20권4호
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    • pp.1501-1509
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    • 1996
  • Differential pressure devices such as an orifice and Venturi are widely used in the measurement of flow rate of fluid mainly due to cost effectiveness and easy installation. In the current study, the viscoelastic effect on discharge and loss coefficients of those flow meters were investigated experimentally. Aqueous solutions of Polyacrylamide (200, 500, and 800 ppm) as viscoelastic fluids were used. Discharge coefficient of an orifice for viscoelastic fluids increased significantly up to approximately 15-20% when compared with that for water, while loss coefficient decreased up to 10-25% depending on the diameter ratio, .betha.. Also, pressure recovery for viscoelastic fluids was extended much longer than that for water. On the other hand, discharge and loss coefficients of Venturi for viscoelastic fluids were found to be strongly dependent on the Reynolds number. In both flow meters, the concentration effect for discharge and loss coefficients was not observed at more over than 200 ppm of aqueous solution. Conclusively, orifice and Venturi flow meters should be calibrated very carefully in the flow rate measurement for viscoelastic fluids.

인젝터 압력이 단공노즐 감압비등 분무에 미치는 영향 (Effect of Injection Pressure on the Flash Boiling Spray from Simple Orifice Nozzle)

  • 이현창;차현우;강동현
    • 한국분무공학회지
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    • 제27권1호
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    • pp.42-49
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    • 2022
  • Flash boiling occurs in a couple of modern engineering systems and understanding its mechanism is important. In this experimental study, discharge coefficient of flash boiling spray from simple orifice nozzle was measured, and backlight imaging was acquired at injection pressure to 6.0 bar and temperature to 163℃ for the purpose. Pressurized water by pump was used for working fluid and was heated by electric heater and ejected through simple orifice nozzle diameter of 0.5 mm. High speed camera with long distance microscope was used for backlight imaging in two FoV having magnification of 3.3 and 0.64. The decrease of discharge coefficient according to degree of superheating and evolution of flash boiling spray imaged at various pressure and temperature were explained by the pressure field inside the injector.

단공 분사기와 압력 선회형 분사기의 내부유동 특성 및 성능해석 (Internal Flow Characteristics & Performance Analysis of Plain Orifice and Pressure Swirl Atomizers)

  • 이장우;황용석;성홍계
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2005년도 제25회 추계학술대회논문집
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    • pp.93-99
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    • 2005
  • 단공 분사기와 선회형 분사기의 두 가지 연료분사기에 대해 2상 유동 수치해석을 수행하였다. 단공 분사기의 경우, 캐비테이션 모델을 적용하여 압력조건에 따른 유출계수, 캐비테이션 발생 영역 크기와 정도를 계산하여 분석하였으며, 실험결과와도 비교하였다. 선회형 분사기에서는 VOF모델을 적용하여 두 가지 형상에 대해 공기코어의 크기, 분무각, 그리고 벽 압력 분포 등을 실험결과와 비교했다.

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노즐 오리피스 형상 및 형상비가 디젤과 바이오디젤 연료의 노즐 내부 및 외부 유동특성에 미치는 영향 (Effect of Nozzle Orifice Shape and Nozzle Length-to-Diameter Ratio on Internal and External Flow Characteristics of Diesel and Biodiesel Fuel)

  • 박수한;서현규;이창식
    • 대한기계학회논문집B
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    • 제31권3호
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    • pp.264-272
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    • 2007
  • The aim of this study is to investigate the effects of nozzle orifice shapes and the nozzle length-to-diameter ratio(L/D) on the nozzle cavitation formation inside the orifice and the external flow pattern. The nozzle used in this work was tested the taper orifice nozzle and the rectangular orifice nozzle which was made from the transparent acrylic acid resin. For studying the effect of the nozzle L/D ratio, it was used to three L/D ratios of 3.33, 10, and 20. The cavitation flow of nozzle was visualized by using the ICCD camera and optical system. This work revealed that the flow rate and discharge coefficient($C_d$) of the taper orifice nozzle was larger than those of the rectangular orifice nozzle at the same injection pressure. The cavitation flow was observed in the nozzle orifice at the low injection pressure and the breakup of liquid jet was promoted as the L/D ratio is decreased. The cavitation of biodiesel fuel was formed at the lower injection pressure than that of diesel fuel because of higher viscosity and density.

전자유압 서보 유량제어밸브의 설계 및 동특성 향상에 관한 연구 (A Study on the Design and the Dynamic Characteristics of Electro-Hydraulic Flow Control Servo Valve)

  • 김고도;김수태
    • 한국정밀공학회지
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    • 제17권2호
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    • pp.151-160
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    • 2000
  • An experimental and theoretical analysis for the improvement of dynamic characteristics and design of electro-hydraulic flow control servo valve are performed. The theoretical results are compared with the experimental step responses, and the important design parameters of an electro-hydraulic flow control servo valve are derived by using the simulation program. Simulation parameters of nozzle jet coefficient and orifice and spool valve discharge coefficient are given through experiment. The theoretical and experimental step response curves show that the valve gain depends on the fixed orifice and nozzle $ratio(R_on)$ and is maximum at $R_on=1.$ And drain orifice in the flapper - nozzle return line creates a small back pressure, which improves the performance fur the valve.

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항공기의 도어 댐퍼용 교축 오리피스의 설계 (Design of Throttle Orifices for an Aircraft Door Damper)

  • 권용철;김종혁;홍예선;김상범
    • 드라이브 ㆍ 컨트롤
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    • 제9권3호
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    • pp.23-28
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    • 2012
  • In this study the flow rate-to-pressure difference characteristics of short-tube type damping orifices for an aircraft door damper were investigated by CFD analyses and experiments. As the design parameters of the damping orifice its diameter, inlet and outlet angle, tube length and the viscosity of the working fluid were taken into consideration. The results showed that the discharge coefficient of the orifices are dependant on the inlet and outlet angle and the oil viscosity, while their length plays an little significant role. Although the short-tube type damping orifice was employed to induce a turbulent flow, their discharge coefficient decreases rapidly as the oil viscosity gets higher than 50mm2/s. Therefore, in order to determine the orifice size, satisfying the working temperature range of the door damper, the oil viscosity as well as the friction force on the damper piston should be kept within proper values. For the verification of the CFD analysis results the actual performance of a door damper was measured and compared with them.