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      KCI등재

      혼합 액체 연료인 항공유의 점화지연시간 측정에 관한 연구

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      https://www.riss.kr/link?id=A103527334

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      다국어 초록 (Multilingual Abstract)

      Jet aviation fuel is one of liquid fuel which are used in aircraft engines. Korean domestic jet fuel, called Jet A-1, is tested for measurement of ignition delay time by using a shock tube manufactured recently. The temperature varies from 680 to 1250 K and the pressure and equivalence ratio of Jet A-1/air are fixed 20 atm and 1.0, respectively, for this experiment. The ignition delay time data of Jet A-1 are compared with those of Jet A, which has similar properties to Jet A-1. The behavior of negative-temperature-coefficient (NTC) is observed in the temperature range 750-900 K. In addition, ignition delay time of iso-octane is measured, which is one of the surrogate components for jet aviation fuel. The experimental data are compared and validated with the previous results from the literatures. A surrogate fuel for the present Jet A-1 consists of 45.2% n-dodecane, 32.1% iso-octane, and 22.7% 1,3,5-trimethylbenzene. The predicted ignition delay time for the surrogate agrees well with the measured one for Jet A-1.
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      Jet aviation fuel is one of liquid fuel which are used in aircraft engines. Korean domestic jet fuel, called Jet A-1, is tested for measurement of ignition delay time by using a shock tube manufactured recently. The temperature varies from 680 to 1250...

      Jet aviation fuel is one of liquid fuel which are used in aircraft engines. Korean domestic jet fuel, called Jet A-1, is tested for measurement of ignition delay time by using a shock tube manufactured recently. The temperature varies from 680 to 1250 K and the pressure and equivalence ratio of Jet A-1/air are fixed 20 atm and 1.0, respectively, for this experiment. The ignition delay time data of Jet A-1 are compared with those of Jet A, which has similar properties to Jet A-1. The behavior of negative-temperature-coefficient (NTC) is observed in the temperature range 750-900 K. In addition, ignition delay time of iso-octane is measured, which is one of the surrogate components for jet aviation fuel. The experimental data are compared and validated with the previous results from the literatures. A surrogate fuel for the present Jet A-1 consists of 45.2% n-dodecane, 32.1% iso-octane, and 22.7% 1,3,5-trimethylbenzene. The predicted ignition delay time for the surrogate agrees well with the measured one for Jet A-1.

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      목차 (Table of Contents)

      • ABSTRACT
      • 1. 서론
      • 2. 실험 방법
      • 3. 실험 결과 및 고찰
      • 4. 결론
      • ABSTRACT
      • 1. 서론
      • 2. 실험 방법
      • 3. 실험 결과 및 고찰
      • 4. 결론
      • References
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      참고문헌 (Reference)

      1 한희선, "충격파관을 이용한 메탄/산소 혼합기의 점화지연시간 측정" 한국연소학회 22 (22): 8-13, 2017

      2 S.S. Vasu, "n-Dodecane oxidation at high-pressures:Measurements of ignition delay times and OH concentration time-histories" 32 : 173-180, 2009

      3 S. Downes, "Uncertainty Estimation of Shock Tube Pressure Steps" 1-4, 2015

      4 S. Dooley, "The experimental evaluation of a methodology for surrogate fuel formulation to emulate gas phase combustion kinetic phenomena" 159 : 1444-1466, 2012

      5 P. Dievart, "The combustion properties of 1,3,5-trimethylbenzene and a kinetic model" 109 : 125-136, 2013

      6 F. Ducourneau, "Spontaneous combustion of rich air-kerosene mixtures" 10 : 11-18, 1974

      7 K. Fieweger, "Shocktube investigations on the self-ignition of hydrocarbon-air mixtures at high pressures" 25 : 1579-1585, 1994

      8 D.F. Davidson, "Shock tube ignition measurements of iso-octane/air and toluene/air at high pressures" 30 : 1175-1182, 2005

      9 J.T. Herbon, "Shock Tube Measurements of CH3+O2 Kinetics and the Heat of Formation of the OH Radical" Stanford University 2004

      10 S.S. Vasu, "Jet fuel ignition delay times: Shock tube experiments over wide conditions and surrogate model predictions" 152 : 125-143, 2008

      1 한희선, "충격파관을 이용한 메탄/산소 혼합기의 점화지연시간 측정" 한국연소학회 22 (22): 8-13, 2017

      2 S.S. Vasu, "n-Dodecane oxidation at high-pressures:Measurements of ignition delay times and OH concentration time-histories" 32 : 173-180, 2009

      3 S. Downes, "Uncertainty Estimation of Shock Tube Pressure Steps" 1-4, 2015

      4 S. Dooley, "The experimental evaluation of a methodology for surrogate fuel formulation to emulate gas phase combustion kinetic phenomena" 159 : 1444-1466, 2012

      5 P. Dievart, "The combustion properties of 1,3,5-trimethylbenzene and a kinetic model" 109 : 125-136, 2013

      6 F. Ducourneau, "Spontaneous combustion of rich air-kerosene mixtures" 10 : 11-18, 1974

      7 K. Fieweger, "Shocktube investigations on the self-ignition of hydrocarbon-air mixtures at high pressures" 25 : 1579-1585, 1994

      8 D.F. Davidson, "Shock tube ignition measurements of iso-octane/air and toluene/air at high pressures" 30 : 1175-1182, 2005

      9 J.T. Herbon, "Shock Tube Measurements of CH3+O2 Kinetics and the Heat of Formation of the OH Radical" Stanford University 2004

      10 S.S. Vasu, "Jet fuel ignition delay times: Shock tube experiments over wide conditions and surrogate model predictions" 152 : 125-143, 2008

      11 V.L. Zimont, "Ignition lag of hydrocarbon fuels at high temperatures" 3 : 51-56, 1967

      12 B.P. Mullins, "Development of a combustion test rig for measuring the ignition delay of fuels" 32 : 234-352, 1953

      13 C.P. Wood, "Development and application of a surrogate distillate fuel" 5 : 399-405, 1989

      14 "Coordinating Support of Fuels and Lubricant Research and Development (R&D) 2"

      15 H. Wang, "Autoignition studies of conventional and Fischer-Tropsch jet fuels" 98 : 249-258, 2012

      16 A.J. Dean, "Autoignition of surrogate fuels at elevated temperatures and pressures" 31 : 2481-2488, 2007

      17 L.J. Spadaccini, "Autoignition characteristics of aircraft-type fuels" 46 : 282-300, 1982

      18 S.R. Turns, "An introduction to combustion" McGraw-Hill 1-676, 2000

      19 H-P.S. Shen, "A shock tube study of iso-octane ignition at elevated pressures: The influence of diluent gases" 155 : 739-355, 2008

      20 S. Dooley, "A jet fuel surrogate formulated by real fuel properties" 157 : 2333-2339, 2010

      21 E.L. Petersen, "A facility for gas-and condensed-phase measurements behind shock waves" 16 : 1716-1729, 2005

      22 H-P.S. Shen, "A Shock Tube Study of the Ignition of n-Heptane, n-Decane, n-Dodecane, and n-Tetradecane at Elevated Pressures" 23 : 2482-2489, 2009

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2022 평가예정 재인증평가 신청대상 (재인증)
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      2012-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2009-01-01 평가 등재학술지 선정 (등재후보2차) KCI등재
      2008-01-01 평가 등재후보 1차 PASS (등재후보1차) KCI등재후보
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      학술지 인용정보

      학술지 인용정보
      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 0.31 0.31 0.29
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.27 0.25 0.632 0.05
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