• Title/Summary/Keyword: Swirl angle

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Effect of Internal Geometry of Nozzle on the Velocity and Droplet Size of Twin Spray (노즐이 내부형상이 이중분무의 유속과 입경에 미치는 영향)

  • Kim, Young-Jin;Jung, Ji-Won;Kim, Duck-Jool
    • Proceedings of the KSME Conference
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    • 2004.04a
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    • pp.1522-1527
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    • 2004
  • The purpose of this study is to investigate the effect of swirler angle and swirl chamber aspect ration of nozzle on the characteristics of single and twin spray. The performances of nozzle has been investigated by measurements of spray angle, droplet size, velocity and Weber number at a water pressure 0.4MHz. Visualization of spray was conducted to obtain the spray angle and breakup process. The spray characteristics such as droplet size and velocity were measured by Phase Doppler Anemometry(PDA). It was found that the smaller swirler angle, the larger axial velocity became. It was also shown that the larger aspect ratio, the smaller droplet diameter became.

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Effects of Combustion Instability by Swirl Intensity in Hybrid Rocket (스월 강도에 따른 하이브리드 로켓의 연소 불안정 영향)

  • Kim, Jungeun;Lee, Sulha;Kim, Ji Eun;Kim, Ji Hye;Yoo, Min Jeong;Han, Songee;Lee, Changjin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.672-674
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    • 2017
  • The addition of swirl is a common technique used in premixed combustors in order to gain stability of the combustion with the improvements in mixing characteristics. recent experimental studies have observed that the addition of swirl oxidizer flow can effectively reduce the combustion instability in hybrid rocket. Investigation was continued to analyze the effect of the swirl on the internal flow of hybrid rocket engine main combustion chamber. The flow influenced by wall blowing as a representation of fuel evaporation interacts with swirling flow. Swirl angle increases, the amplitude of the combustion pressure decrease as the unstable combustion processes. These results suggest that the oxidizer swirling flow by the swirl angle causes the change of the turbulent flow characteristics inside the combustion chamber and suppresses the factors causing the combustion instability.

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Numerical analysis on the characteristics of disel spray for variation of injection spray angle and swirl ratio. (분사각 및 스월 변화에 따른 디젤분무의 특성에 관한 수치 해석)

  • Jung H.;Cha K. S.;Park C. G.
    • Journal of computational fluids engineering
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    • v.5 no.3
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    • pp.1-7
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    • 2000
  • In high-pressure diesel engine, the injected fuel spray impinges on the piston cavity surface due to the short distance between the injection nozzle and the cavity wall. The behavior of the impinging spray has the great influence on the dispersion of fuel, the evaporation, and the mixture formation process. In this study, the numerical simulation using the GTT code was performed to study the gas flows, the spray behaviors, and the fuel vapor distributions in the combustion of a D.I engine for variation of spray angle and swirl ratio.

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Flow Analysis for Optimum Design of Mixing Vane in a PWR Fuel Assembly

  • In, Wang-Kee;Oh, Dong-Seok;Chun, Tae-Hyun
    • Nuclear Engineering and Technology
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    • v.33 no.3
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    • pp.327-338
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    • 2001
  • A computational fluid dynamics (CFD) analysis was performed to propose the optimum design of flow mixing vane on the space grid in a PWR fuel assembly. The flow mixing vanes considered in this study for optimum design are swirl-vane and twisted-vane. A single subchannel of one grid span was modeled using flow symmetry to minimize the computational effort. The CFD predictions are in good agreement with the experimental results for the split- vane, which shows the applicability of the CFD method. The mixing effect by swirling flow and crossflow, and the pressure drop were estimated and compared for the various vane angles. The optimum vane angle is proposed to be 40。 and 35。 from the direction of axial flow for the swirl-vane and the twisted-vane, respectively.

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Experimental Study on Recess Characteristic of Swirl Coaxial Injector (스월 동축형 인젝터의 리세스 특성에 대한 실험적 연구)

  • Choi, Ho-Yeon;Kim, Sung-Hyuk;Yoon, Jung-Soo;Yoon, Yung-Bin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.217-220
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    • 2009
  • This paper presents experimental results of Recess Characteristic of Swirl Coaxial Injector of fuel-rich gas generators. It was revealed that the internal impinging phenomenon played an important role in the spray characteristics, such as spray angle and breakup length.

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Effects of the Bio-diesel Blending Rate on the Spray Characteristics of the Pressure Swirl Nozzle (바이오 디젤 혼합율이 압력식 스월노즐의 분무 특성에 미치는 영향)

  • Yoon, S.J.
    • Journal of ILASS-Korea
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    • v.16 no.4
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    • pp.210-214
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    • 2011
  • This paper presents the spray characteristics of the gun type burner nozzle with bio-diesel blending rate. The burner nozzle used in this experiment is a pressure swirl type nozzle. For the spray characteristics, visualization of spray was conducted to obtain the spray angle, and laser diffraction spectroscope (LDS) was used for the measurement of the droplet diameters. The results showed that the $D_{max}$, SMD and spray angle were decreased with increasing the bio-diesel blending rate and BD30 (30% bio-diesel blending rate) could be found to be the maximum blending rate for using without any modification of the gun type burner of the homesize kerosene fuel boiler.

Comparison of Spray Characteristics between Conventional and Electrostatic Pressure-Swirl Nozzles

  • Laryea, G.N.;No, S.Y.
    • Journal of ILASS-Korea
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    • v.11 no.1
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    • pp.24-29
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    • 2006
  • Spray characteristics produced by conventional and electrostatic pressure-swirl nozzles for an oil burner have been studied, using kerosine as a test liquid. The charge injection mechanism is used to design the electrostatic nozzle, where specific charge density, breakup length, spray angle and mean diameter are measured and analyzed. Three nozzles with orifice diameters of 0.256, 0.308 and 0.333mm at injection pressures of 0.7, 0.9, 1.1 and 1.3 MPa are used in the study. In case of the electrostatic nozzle, voltages ranging from -5 to -12kV are applied. Comparison of the spray characteristics is made between the conventional and electrostatic nozzles. The results showed that, the electrostatic nozzle is superior to the conventional nozzle. This is due the effect of voltage on the liquid surface tension.

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EXPERIMENTAL STUDY ON TURBULENT SWIRLING FLOW IN A CYLINDRICAL ANNULI BY USING THE PIV TECHNIQUE

  • Chang, T.H.
    • International Journal of Automotive Technology
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    • v.5 no.1
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    • pp.17-22
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    • 2004
  • An experimental investigation was conducted to study the characteristics of turbulent swirling flow in an axisymmetric annuli. The swirl angle measurements were performed using a flow visualization technique using smoke and dye liquid for Re=60,000-80,000. Using the two-dimensional Particle Image Velocimetry method, this study found the time-mean velocity distribution and turbulence intensity in water with swirl for Re=20,000, 30,000, and 40,000 along longitudinal sections. There were neutral points for equal axial velocity at y/(R-r)=0.7-0.75, and the highest axial velocity was recorded near y/(R-r)=0.9. Negative axial velocity was observed near the convex tube along X/(D-d)=3.0-18.0 for Re=20,000.

A Study on Combined Effects between Swirl and Tumble Flow of Intake Port System in Cylinder Head (엔진 흡입포트 시스템 유동특성 규명을 위한 스월-텀블 합성효과에 관한 연구)

  • 윤정의
    • Transactions of the Korean Society of Automotive Engineers
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    • v.7 no.8
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    • pp.76-82
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    • 1999
  • The object of this study is to find new evalution index for in-cylinder flow characteristics insteady of current swirl, tumble coefficient using steady flow test rig on intake port system. To this end, port flow rig test was conducted on DOHC head varying intake valve lift respectively. Finally combination angular coefficient and inclination angle were introduced as new evaluation index for in-cylinder angular flow characteristics.

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In-Cylinder Phenomena in a Swirl Type GDI Engine (스월형 GDI 엔진의 연소실내 현상 연구)

  • 김기성;박상규
    • Proceedings of the Korean Society of Marine Engineers Conference
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    • 2001.05a
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    • pp.75-90
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    • 2001
  • For the purpose of helping development of a GDI(Gasoline Direct Injection) engine, the in-cylinder phenomena, such as the spray behaviors and fuel distributions, unburned fuel, and flame characteristics were investigated in a single cylinder GDI engine. The GDI engine was equipped with a swirl type electronic injector and SCV(Swirl Control Valve). PLIF(Planar Laser Induced Fluorescence) system with KrF Excimer laser was used for the measurements of the fuel distributions. The effects of the injector specifications, such as the spray cone angle and the offset angle on the fuel distributions and combustion characteristics were investigated. As a result, it was found that the injected fuel spray collided with the bottom of the bowl and moved upward along the exhaust side wall of the piston bowl. This fuel vapor played a important role in the instance of spark ignition. The injector specifications has a great influence on the flame characteristics.

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