• 제목/요약/키워드: High Ambient Pressure

검색결과 329건 처리시간 0.025초

분위기 조건이 Decane 액적의 Soot 생성에 미치는 영향 (Effect of Ambient Conditions on the Soot Generation of Decane Fuel Droplet)

  • 임영찬;서현규
    • 한국분무공학회지
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    • 제19권4호
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    • pp.211-215
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    • 2014
  • The main purpose of this study is to provide basic information of droplet soot generation of decane fuel. To achieve this, this paper presents the experimental results on the decane droplet combustion conducted under various ambient pressure($P_{amb}$), and oxygen concentration($O_2$) conditions. At the same time, the experimental study was conducted in terms of soot volume fraction($f_v$) and its maximum value. Also, visualization of single fuel droplet was conducted by high resolution CCD camera and ambient pressure($P_{amb}$) and oxygen concentration($O_2$) was changed by control system. It was revealed that higher ambient pressure($P_{amb}$), and oxygen concentration($O_2$) enhanced the soot generation and improved the maximum soot volume fraction( $f_v$).

탄화수소 연료 액적의 연소 특성에 관한 수치해석 (A Numerical Study of Combustion Characteristics of Hydrocarbon Fuel Droplet)

  • 이봉수;이경재;김종현;구자예
    • 대한기계학회논문집B
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    • 제27권11호
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    • pp.1595-1603
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    • 2003
  • Droplet combustion at high ambient pressures is studied numerically by formulating one dimensional combustion model in the mixture of n-heptane fuel and air. The ambient pressure is supercritical conditions. The modified Soave-Redlich-Kwong state equation is used in the evaluation of thermophysical properties to account for the real gas effect on fluid p-v-T properties in high pressure conditions. Non-ideal thermodynamic and transport property at near critical and supercritical conditions are also considered. Several parametric studies are performed by changing ambient pressure and initial droplet diameter. Droplet lifetime decreased with increasing pressure. Surface temperature increased with increasing pressure. Ignition time increased with increasing initial droplet diameter. Temporal or spatial distribution of mass fraction, mass diffusivity, Lewis number, thermal conductivity, and specific heat were presented.

Development Behavior of Vaporizing Sprays from a High-Pressure Swirl Injector Using Exciplex Fluorescence Method

  • Choi, Dong-Seok;Kim, Duck-Jool;Hwang, Soon-Chul
    • Journal of Mechanical Science and Technology
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    • 제14권10호
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    • pp.1143-1150
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    • 2000
  • The effects of ambient conditions on vaporizing sprays from a high-pressure swirl injector were investigated by an exciplex fluorescence method. Dopants used were 2% fluorobenzene and 9% DEMA (diethyl-methyl-amine) in 89% solution of hexane by volume. In order to examine the behavior of liquid and vapor phases inside of vaporizing sprays, ambient temperatures and pressures similar to engine atmospheres were set. It was found that the ambient pressure had a significant effect on the axial growth of spray, while ambient temperature had a great influence on the radial growth. The spatial distribution of vapor phase at temperatures above 473K became wider than that of liquid phase after half of injection duration. From the analysis of the area ratio for each phase, the middle part (region II) in the divided region was the region which liquid and vapor phases intersect. For liquid phase, fluorescence-intensity ratio was greatly changed at lms after the start of injection. However, the ratio of vapor phase was nearly uniform in each divided region throughout the injection.

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고압에서의 분무의 증발 및 연소 현상에 관한 연구 (Study on Vaporization and Combustion of Spray in High Pressure Environment)

  • 왕태중;백승욱
    • 대한기계학회논문집B
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    • 제27권9호
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    • pp.1273-1281
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    • 2003
  • The present study is mainly motivated to investigate the vaporization, auto-ignition, and combustion of liquid fuel spray injected into high pressure environment. The unsteady, multi-dimensional models were used for realistic simulation of spray as well as prediction of accurate ignition delay time. The Separated Flow (SF) model which considers the finite rate of transport between liquid and gas phases was employed to represent the interactions between spray and gas field. Among the SF models, the Discrete Droplet Model (DDM) which simulates the spray using finite number of representative samples of discrete droplets was adopted. The Eulerian-Lagrangian formulation was used to analyze the two-phase interactions. In order to predict an evaporation rate of droplet in high pressure environment, the high pressure vaporization model was applied using thermodynamic equilibrium and phase equilibrium at droplet surface. The high pressure effect as well as high temperature effect was considered in the calculation of liquid and gas properties. In case of vaporization, an interaction between droplets was studied through the simulation of spray. The interaction is shown up differently whether the ambient gas field is at normal pressure or high pressure. Also, the characteristics of spray behavior in high pressure environment were investigated through the comparison with normal ambient pressure case. In both cases, the spray behaviors are simulated through the distributions of temperature and reaction rate in gas field.

Spray Characteristics of the Rocket Oxidizer-rich Preburner Injection System

  • Yang, Joon-Ho;Choi, Seong-Man;Han, Young-Min
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년 영문 학술대회
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    • pp.255-259
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    • 2008
  • This paper presents the spray characteristics of the oxidizer rich preburner injector which can be used in the high-thrust rocket system. We designed the basic shape of the liquid-liquid coaxial swirl injector for the rocket oxidizer rich preburner injection system. To understand the spray angle variation with the high pressure environment, the spray visualization in the high pressure chamber was preformed. Also we measured the droplet velocity, the Sauter Mean Diameter(SMD), the volume flux and the number density with the PDPA system by using water in atmospheric pressure. The results show that the spray angle is reduced by increasing ambient pressure and maximum droplet velocity is shown from a nozzle tip and then the droplet velocity decreases as a spray moves to the downstream. The SMD decreases on the axial distance from 20 mm to 50 mm but it increases over 50 mm. That is due to the increasing number of collision with each droplet and interaction with ambient air on going downstream direction.

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고압 환경에서의 분무 특성 계측을 위한 광학 토모그래피 기법 연구 (Study of Optical Tomography for Measurement of Spray Characteristics at High Ambient Pressure)

  • 조성호;임지혁;최호연;윤영빈
    • 한국추진공학회지
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    • 제13권4호
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    • pp.36-44
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    • 2009
  • 광학 선형 패터네이터 및 광학 토모그래피 기법을 사용하여 높은 주위 기체 압력 조건에서 분무단면을 측정하였다. 레이저 직선광이 분무 영역을 지나도록 하여 발생하는 Mie 산란 신호 및 직선광의 투과율을 측정하였으며, 이로부터 Beer-Lambert 법칙 및 수학적 단면 재구성 기법을 이용하여 분무 단면의 감쇠 계수 분포를 재구성하였다. 높은 주위 기체 압력 조건에서 광학적으로 밀한 분무가 발생하며, 그 결과 산란 신호의 감쇠 효과가 크게 증가한다. 따라서 미 산란 신호를 이용하는 광학 선형 패터네이터의 경우 감쇠 효과를 완화하는 데 한계를 보인다. 광학 토모그래피의 경우 분무를 통과하는 레이저광의 투과율 정보만을 이용하여 성공적으로 분무 단면을 재구성하였다.

고압환경에서 동축 와류형 분사기의 분무특성 (Spray Characteristics of Coaxial Swirl Injector under Ambient High Pressure Conditions)

  • 임병직;김종규;문일윤;김승한;한영민;설우석
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제23회 추계학술대회 논문집
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    • pp.288-291
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    • 2004
  • 본 논문은 고압조건에서 동축 와류형 분사기의 분무특성 파악을 위한 연구로서 3종류의 분사기가 사용되었으며, 함몰길이와 연료 분사기의 형태에 따른 분무특성을 확인하였다. 또한, 실제 연소기에 서 발생되는 연소압력과 수류 실험에서의 압력 상사조건을 계산하여 실험을 수행하여 분사압에 따른 유량변화, 분무각, 질량분포, 평균 액적크기 등의 분무특성이 측정되었다.

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증착조건에 따른 undoped ZnO 박막의 특성 변화 (Property variations of undoped ZnO thin films with deposition conditions)

  • 남형진;이규항;조남인
    • 반도체디스플레이기술학회지
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    • 제7권3호
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    • pp.51-54
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    • 2008
  • In this study, we investigated variations in undoped ZnO thin film properties with working pressure, $O_2$/Ar ratio, and annealing ambient. Higher vacuum pressure during deposition was observed to bring about slower growth rate resulting in samples with better crystallinity as well as hole generation efficiency through formation of shallower oxygen interstitial. Given that $O_2$/Ar ratio is greater than unity, O provided from the ambient to ZnO during annealing was found to preferably situate at interstitial sites. When He was used for the second annealing, significant changes were not observed. On the other hand, O ambient caused increased density of oxygen interstitial, thereby making the film more intrinsic-like high resistivity ZnO.

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일차원 액적 배열하에서 화염 퍼짐에 관한 실험적 연구 (An Experimental Study on Flame Spread in an One-Dimensional Droplet Array)

  • 박정;신현동;코바야시 히데아키;니오카 다카시
    • 대한기계학회논문집B
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    • 제23권1호
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    • pp.131-139
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    • 1999
  • Experimental investigations on flame spread in droplet arrays have been conducted under supercritical ambient pressures of fuel droplet. Flame spread rates are measured for n-Decane droplet of diameters of 0.75 and 1.0mm, using high speed images of OH chemiluminescence up to 3.0MPa. The pattern of flame spread is categorized into two: a continuous mode and an intermittent one. There exists a limit droplet spacing, above which flame spread does not occur. Flame spread rate with the decrease of droplet spacing increases and then decreases after takin& a maximum. It is also seen that there exists a limit ambient pressure, above which flame spread does not occur. Flame spread rate decreases monotonically with the increase of ambient pressure. Exceptionally, In the case of a small droplet spacing, flame spread with the increase of ambient pressure is extended to supercritical pressures of fuel droplet. This is caused by enhanced vaporization with the increase of ambient pressure. Consequently, in flame spread with droplet droplet spacing, the relative position of flame to droplet spacing plays an important role. The monotonic decrease with ambient pressure is mainly related to the reduction of flame radius in subcritical pressures and the extension to supercritical pressures of flame spread is caused by the reduction of ignition time of unburnt droplet due to the enhanced vaporization at supercritical pressures.

SUPERBUBBLES AS SPACE BAROMETERS

  • GARCIA-SEGURA G.;OEY M. S.
    • 천문학회지
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    • 제37권4호
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    • pp.217-222
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    • 2004
  • High ambient interstellar pressure is suggested as a possible factor to explain the ubiquitous ob-served growth-rate discrepancy for supernova-driven super bubbles and stellar wind bubbles. Pressures of P / k ${\~} 10^5\;cm^{-3}$ K are plausible for regions with high star formation rates, and these values are intermediate between the estimated Galactic mid-plane pressure and those observed in starburst galaxies. High-pressure components also are commonly seen in Galactic ISM localizations. We demonstrate the sensitivity of shell growth to the ambient pressure, and suggest that super bubbles ultimately might serve as ISM barometers.