• Title/Summary/Keyword: Momentum ratio

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Effect of Weber Number and Momentum Flux Ratio on Macroscopic Characteristics of Spray from a Coaxial Porous Injector (웨버수 및 운동량 플럭스비에 따른 동축형 다공성재 분사기의 거시적 분무특성)

  • Kim, Do-Hun;Seo, Min-Kyo;Lee, In-Chul;Koo, Ja-Ye
    • Journal of the Korean Society of Propulsion Engineers
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    • v.16 no.5
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    • pp.1-9
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    • 2012
  • The gas jet from a coaxial porous injector for two-phase flows is discharged from the porous surface, which encloses the center liquid jet, and the gas and liquid jet interact with each other physically. The wall injected gas jet transfers the radial momentum effectively while the radial gas jet develops to axial jet, and the performance of atomizing and mixing can be improved. In this study, the Weber number and the ratio of momentum flux were controlled by changing the gas injection area and the mass flow rate of the gas jet, and a study on the spray characteristics at the cold-flow test using water and air simulant was performed. It is concluded that the radial momentum transfer concept of a coaxial porous injector gives a positive effect on the atomization and mixing of the two-phase spray.

The Experimental Study on the Lift-off Height due to Momentum Ratio in Swirl-Coaxial Injector (2유체 동축인젝터의 공급 운동량비가 화염부상거리에 미치는 영향에 관한 실험적 연구)

  • Moon, I.Y.;Kim, Y.;Park, H.H.;Kim, S.J.
    • Journal of the Korean Society of Propulsion Engineers
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    • v.4 no.1
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    • pp.30-35
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    • 2000
  • The experimental study on the lift-off height of diffusion flames was conducted to investigate the damage of swirl-coaxial injector used in $GO_2$/kerosene rocket engine during initial stage of ignition. To investigate the causes of damage and to prevent further damage of the injector, experimental injector was designed and hot fire tests were performed with varying propellant momentum ratio($\frac{Momentum of {GO_2}}{Momentum of Kerosene}$) from 1 to 12. In experimental coaxial injector, kerosene is sprayed from the central nozzle with swirl and $GO_2$ sprayed around the kerosene nozzle in the direction parallel to the axis of combustion chamber. Chamber pressure are close to the atmospheric condition. Lift-off height was measured by still images from camcoder and average values were used as data.

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Contrarian Strategy Based on Past Stock Return and Volatility (변동성을 이용한 반대투자전략에 대한 실증분석)

  • Park, Kyeong-In;Jee, Chang
    • The Korean Journal of Financial Management
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    • v.23 no.2
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    • pp.1-25
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    • 2006
  • This paper studied the performance of momentum strategy and contrarian strategy based or past stock return ratio of Korean stock market. The comparative study shows that the volatility of stock markets that can be found the performance of momentum strategy is smaller than that of emerging stock market. Accordingly, This paper examines that the performances of momentum strategy and contrarian strategy are affected by the larger volatility in Korean stock market. Further analysis using the 6 years sub-portfolios reveals that the momentum strategy is significant only during 1980 to 1986 time period when it had the least market volatility. Additionally, we investigate whether firm-level volatility as well as market volatility influence on the performance of contrarian strategy, and figure out that the momentum strategy is significant for the portfolio composed of firms with smaller volatility for previous period, while not significant for the portfolio composed of firms with larger volatility.

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Friction of a Brownian Particle in a Lennard-Jones Solvent: A Molecular Dynamics Simulation Study

  • Lee, Song-Hi
    • Bulletin of the Korean Chemical Society
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    • v.31 no.4
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    • pp.959-964
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    • 2010
  • In this work, equilibrium molecular dynamics (MD) simulations in a microcanonical ensemble are performed to evaluate the friction coefficient of a Brownian particle (BP) in a Lennard-Jones (LJ) solvent. The friction coefficients are determined from the time dependent friction coefficients and the momentum autocorrelation functions of the BP with its infinite mass at various ratios of LJ size parameters of the BP and solvent, ${\sigma}_B/{\sigma}_s$. The determination of the friction coefficients from the decay rates of the momentum autocorrelation functions and from the slopes of the time dependent friction coefficients is difficult due to the fast decay rates of the correlation functions in the momentum-conserved MD simulation and due to the scaling of the slope as 1/N (N: the number of the solvent particle), respectively. On the other hand, the friction coefficient can be determined correctly from the time dependent friction coefficient by measuring the extrapolation of its long time decay to t=0 and also from the decay rate of the momentum autocorrelation function, which is obtained by time integration of the time dependent friction coefficient. It is found that while the friction coefficient increases quadratically with the ratio of ${\sigma}_B/{\sigma}_s$ for all ${\sigma}_B$, for a given ${\sigma}_s$ the friction coefficient increases linearly with ${\sigma}_B$.

Characteristic of Liquid Jet in Subsonic Cross-flow (횡단가스 유동에 분사되는 액체제트의 분무특성)

  • Ko, Jung-Bin;Lee, Kwan-Hyung;Koo, Ja-Ye
    • Journal of ILASS-Korea
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    • v.10 no.1
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    • pp.35-42
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    • 2005
  • The present study has numerically and experimentally investigated the spray behavior of liquid jet injected in subsonic cross-flow. The corresponding spray characteristics are correlated with jet operating parameters. The spray dynamics are known to be distinctly different in the three regimes: the column, the ligament and the droplet regimes. The behaviors of column, penetration and breakup of liquid jet have been studied. Numerical and physical models are base on a modified KIVA code. The primary atomization is represented by a wave model base on the KH(Kelvin-Helmholtz) instability that is generated by a high interface relative velocity between the liquid and gas flows. In odor to capture the spray trajectory, CCD camera has been utilized. Numerical and experimental results indicate that the breakup point is delayed by increasing gas momentum ratio and the penetration decreases by increasing Weber number.

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Development of the Natural Gas Burner for Modified Chemical Deposition Processes (화학증착용 천연가스버너 개발)

  • You, Hyun-Seok;Lee, Joong-Seong;Han, Jeong-Ok;Choi, Dong-Soo
    • 한국연소학회:학술대회논문집
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    • 2001.06a
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    • pp.75-81
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    • 2001
  • MCVD(modified chemical vapor deposition) used in making optical-fiber currently utilizes the hydrogen-oxygen burner as a energy supply source. To improve the productivity and to reduce the manufacturing cost of optical-fiber, a natural gas-oxygen burner has been developed. The manufacturing processes of optical-fiber consist of vapor deposition, collapse and drawing processes. Among these processes, the vapor deposition and the collapse processes are important in terms of improving the productivity and saving the production cost. The vapor deposition and collapse processes are performed by combustion heat and flame force supplied by a burner. So the flame force of the burner used in these processes is required to have an optimal and consistent value in order to allow uniform heating and collapse of quartz tube. In this regard, the momentum ratio of natural gas and oxygen has been optimally determined by modification of a burner and the inlet flow pass also has been modified.

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Study on Heat Transfer around a Circular Jet Ejected into a Supersonic Flow (초음속 유동내에 분사되는 원형 제트 주위에서의 열전달 연구)

  • Yi, Jong-Ju;Yu, Man-Sun;Cho, Hyung-Hee
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.11a
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    • pp.353-356
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    • 2006
  • Convective heat transfer coefficient was measured around a secondary jet ejected into the supersonic flow field. Wall temperature distribution was measured on the surface, which the constant heat flux condition is applied. According to jet to freestream momentum ratio, the secondary flow was penetrated into the supersonic flow field. During the test, two dimensional thermal image of a wall temperature is taken by an infra-red camera. Experiments were performed under the testing condition of freestream Mach number of about 3, stagnation pressure of 630 kPa and Reynolds number of $3.0{\times}10^6$.

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Atomization Characteristics of a Double Impinging F-0-0-F Type Injector with Four Streams for Liquid Rockets

  • Kang, Shin-Jae;Rho, Byung-Joon;Oh, Je-Ha;Kwon, Ki-Chul
    • Journal of Mechanical Science and Technology
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    • v.14 no.4
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    • pp.466-476
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    • 2000
  • This paper presents atomization characteristics of a double impinging F -0-0- F type injector with four streams. A phase Doppler particle analyzer was employed to measure the droplet-size and water was used as the inert simulant liquid instead of reactive propellant liquids. The droplet mean diameter (SMD) and size distribution were measured to investigate the effects of the momentum ratio and pressure drop variations. This experimental results can be used during the preliminary design stage of a impinging stream type injector for liquid rockets.

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Effects of Propellant Phases on Atmospheric Spray Characteristics of a Pintle Injector for Throttleable Rocket Engines (가변 추력용 핀틀 분사기에서 추진제 상에 따른 상압분무 특성)

  • Yu, Kijeong;Son, Min;Radhakrishnan, Kanmaniraja;Kim, Heuy Dong;Koo, Jaye
    • Journal of ILASS-Korea
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    • v.21 no.1
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    • pp.13-19
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    • 2016
  • Atmospheric spray characteristics were experimentally compared between liquid-gas and liquid-liquid sprays of a pintle injector. In order to study spray characteristics, water and air were used as the simulants and the visualization technic was adopted. Spray images were acquired by using a backlight method by a high-resolution CMOS camera. As a result, when the pintle opening distance increased, liquid sheets became unstabled and fluttering droplets increased. In the liquid-gas case, the breakup performance increased as the pressure of gas injected from the annular orifice increased. In the liquid-liquid case, atomization efficiency decreased as the pressure of liquid injected from the annular orifice increased. Spray angles presented a similar trend between two cases. At the same momentum ratio, the spray angle of liquid-liquid case was lower than the angle of liquid-gas case.

Study on the Surface Heat Transfer Around a Circular Secondary Jet in the Supersonic Flow (초음속 유동내 원형 2차분사 제트 주변에서의 표면 열전달 현상 연구)

  • Yi, Jong-Ju;Yu, Man-Sun;Cho, Hyung-Hee
    • Journal of the Korean Society of Propulsion Engineers
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    • v.11 no.2
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    • pp.47-53
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    • 2007
  • Convective heat transfer coefficient was measured around a circular secondary jet ejected into the supersonic flow field. The wall temperature measurement around a injection nozzle was conducted using infra-red camera. The constant heat flux is applied to the wall around a secondary nozzle. According to jet to freestream momentum ratio, the injection flow penetrates into the supersonic flow field. The measured temperature is used to calculate the convective heat transfer coefficient.