• Title/Summary/Keyword: Spray Model

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CONDITIONAL MOMENT CLOSURE MODELING OF TURBULENT SPRAY COMBUSTION IN A DIRECT INJECTION DIESEL ENGINE

  • HAN I. S.;HUH K. Y.
    • International Journal of Automotive Technology
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    • v.6 no.6
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    • pp.571-577
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    • 2005
  • Combustion of turbulent sprays in a direct injection diesel engine is modeled by the conditional moment closure (CMC) model. The CMC routines are combined with the KIVA code to provide conditional flame structures to determine mean state variables, instead of mean reaction rates. An independent transport equation is solved for each flame group with equal mass of sequentially evaporating fuel vapor. CMC calculation begins as the fuel mass for each flame group begins to evaporate with corresponding initialization conditions. Comparison is made with measured pressure traces for four operating conditions at different rpm's and injection conditions. Results show that the CMC model with multiple flame histories can successfully be applied to ignition and mixing-controlled combustion phases of a diesel engine.

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

  • Lee Jang-Woo;Hwang Yong-Seok;Sung Hong-Gye
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2005.11a
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    • pp.93-99
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    • 2005
  • Performed were 2-phase numerical studies on two types of fuel atomizers, plain orifice and pressure swirl atomizer. In case of plain orifice, cavitation model was applied so that discharge coefficient, cavitation size, and magnitude of cavitation region characterized and compared with experimental results for several different pressure enforced to the orifice. In case of swirl atomizer, VOF model was applied to analyze air core size, spray angle, and wall pressure distributions with comparison of experimental results.

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Thermodynamic model of one of the super heaters and the related spray in the Nekka power plant and Presenting SCO method to control boiler temperature

  • Zalloi, Mehdi;Barghandan, Saeed;Badamchizadeh, M.A.
    • 제어로봇시스템학회:학술대회논문집
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    • 2005.06a
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    • pp.129-133
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    • 2005
  • In this paper, first the thermodynamic model is presented to one of the super heaters and sprays of the Nekka power plant and then its unknown parameters are identified according to the registered data of the power plant. SCO control method is introduced to control the external steam temperature of super heater. Finally the conventional method in power plant for controlling external steam temperature of super heater is compared with new method and their performances are presented..

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A Study on the Characteristics of an Oscillating Fluidic Atomizer

  • Kim, K.H.;Kiger, K.;Lee, W.
    • Journal of ILASS-Korea
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    • v.11 no.2
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    • pp.105-112
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    • 2006
  • A unique feature of fluidic atomizers is that the nozzle geometry produces a thin capillary Jet which is forced to oscillate on a 2-dimensional plane through the use of a passive feedback mechanism. The objective of the current work is to characterize the influence of the stagnation pressure at the nozzle exit, jet oscillation and stretching on the breakup properties of the capillary ligament. To achieve this, shadow graph technique is used to measure size, shape, velocity and the number density of the droplets as a function of the position within the spray fan. The breakup length, defined as the radial distance from the breakup point, is analyzed as a function of the non-dimensional parameters. Finally, a kinematic model is developed to simulate the breakup of the oscillating jets at low stagnation pressures. Using the existing jet breakup theories, the model is used to predict the size and diameter distribution of the droplets after primary atomization.

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Integrated CFD on Atomization Process of Lateral Flow in Injector Nozzle

  • Ishimoto, Jun
    • 한국전산유체공학회:학술대회논문집
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    • 2006.10a
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    • pp.7-8
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    • 2006
  • The governing equations for high-speed lateral atomizing injector nozzle flow based on the LES-VOF model in conjunction with the CSF model are presented, and then an integrated parallel computation are performed to clarify the detailed atomization process of a high speed nozzle flow and to acquire data which is difficult to confirm by experiment such as atomization length, liquid core shapes, droplets size distributions, spray angle and droplets velocity profiles. According to the present analysis, it is found that the atomization rate and the droplets-gas two-phase flow characteristics are controlled by the turbulence perturbation upstream of the injector nozzle, hydrodynamic instabilities at the gas-liquid interface, shear stresses between liquid core and periphery of the jet. Furthermore, stable and a high-resolution computation can be attained in the high density ratio (pl/ pg = 554) conditions conditions by using our numerical method.

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A Numerical Study of the Spray Characteristics of Co-axial Swirl Injector in Liquid Propellant Rocket Engine (액체로켓엔진에서 동축 스월형 분사기의 분무특성에 대한 수치적 고찰)

  • Moon Yoon-Wan;Seol Woo-Seok;Yoon Young-Bin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.05a
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    • pp.156-160
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    • 2006
  • This study investigated the characteristics of spray generated by a liquid-liquid co-axial swirl injector used in a combustor of the liquid rocket engine. The linear stability analysis[1] was introduced In liquid sheet breakup and Post[2]'s collision model which considers shattering was adopted on the collision model after breakup. Every model was implemented to KIVA[3], which was adopted as solve. To validate the implemented models the cases of high and low injection velocity were calculated respectively and each result agreed well with test results.

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Analytical Study on Unsteady Flow Characteristics of Urea-SCR Single Hole Injector depend on Nozzle Shape Change (Urea-SCR 단홀 Injector 노즐형상 변화에 따른 비정상유동특성의 해석적 연구)

  • Hwang, Jun Hwan;Park, Sung-Young
    • Journal of ILASS-Korea
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    • v.24 no.3
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    • pp.105-113
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    • 2019
  • In this paper, a study of Urea-SCR System for Dosing Injector for responding to enhanced environmental regulations has been conducted. There is a limit to the experimental approach due to the structural characteristics of the injector. In order to overcome this problem, The analysis was performed assuming unsteady turbulent flow through computational fluid analysis and the internal flow characteristics of the injector were analyzed. By changing the nozzle shape of the injector, the performance factors of the swirl injector by shape were selected and compared. The design parameters were modified by changing the diameter of the nozzle at a constant ratio compared to the base model. Swirl coefficient, outlet mass flow, and sac volume were selected as performance parameters of the injector. The Conv. model to which the taper was applied showed the dominance in mass flow rate, discharge coefficient and swirl because of the smooth fluid flow by shape. Swirl coefficient, outlet mass flow, and sac volume were selected as performance parameters of the injector. As a result of the comparison coefficient derivation with those performance parameters for comparing the performance of the model-specific injector, the Conv-140 model with the nozzle diameter expanded by 140% showed the best value of the comparison coefficient.

Spray and Combustion Characteristics of Liquid Jet in Cross Flow (횡단류에 분사되는 액체 제트의 분무 및 연소 특성)

  • Lee, Gwan-Hyeong;Kim, Du-Man;Gu, Ja-Ye;Hwang, Jin-Seok
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.34 no.12
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    • pp.48-58
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    • 2006
  • The spray and combustion characteristics of liquid jet in cross flow with variation of injection angle are numerically studied. Numerical analysis was carried out using KIVA code, which may be used to generate numerical solutions to spray and chemical reactive fluid problem in three space dimensions and modified to be suitable for simulating liquid jet ejected into the cross flow. Wave model and Kelvin- Helmholtz(KH) /Rayleigh-Taylor(RT) hybrid model were used for the purpose of analyzing liquid column, ligament, and the breakup of droplet. Penetration length increases as flow velocity decreases and injection velocity increases. Numerical error increases as inflow velocity increases. The results of flame propagation contour in combustion chamber and local temperature distribution, combustion emissions were obtained.

Low-Temperature Microencapsulation of Sesame Oil Using Fluidized Bed Granulation (Fluidized bed granulation을 이용한 참기름의 저온 미세캡슐화)

  • Jeong, Chan-Min;Lee, Min-Kyung;Lee, Hyun-Ah;Park, Ji-Yong
    • Korean Journal of Food Science and Technology
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    • v.41 no.1
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    • pp.27-31
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    • 2009
  • Top spray-drying method is frequently utilized for flavor encapsulation, but the top spray-dried products frequently suffer from high losses of volatile flavor as the result of a high processing temperature (150-$300^{\circ}C$). In an effort to solve these problems, a low-temperature fluidized-bed granulating method was utilized to encapsulate the flavor. For the encapsulation of sesame oil, oil-in-water emulsions of sesame oil and a mixture of maltodextrin, modified starch, gum arabic, and gellan gum were bottom-sprayed at milder temperatures (70-$100^{\circ}C$) using a fluidized-bed granulator. Sesame oil extracts from microcapsules were obtained via a simultaneous distillation/extraction technique, and the retention of volatile flavor compounds was analyzed via a gas chromatography-mass spectrometry. The retention of volatile flavors of sesame oil per se, spray-dried and fluidized-bed granulated microcapsules after 3-day-storage at $37^{\circ}C$ were 0.8%, 37.2%, and 42.0%, respectively. In addition, the low-temperature fluidized-bed granulation showed higher encapsulation yield and sensory preferences for the application of commercial products (beef rice porridge), as compared to spray drying.