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      다국어 초록 (Multilingual Abstract)

      As hypersonic flight speeds and engines efficiencies increase, heat loads on an aircraft and it’s engine increase. Because the temperature of the air flow is too high to cool the aircraft structure at hypersonic flight speeds, it is essential to use...

      As hypersonic flight speeds and engines efficiencies increase, heat loads on an aircraft and it’s engine increase. Because the temperature of the air flow is too high to cool the aircraft structure at hypersonic flight speeds, it is essential to use the aircraft fuel as the primary coolant. Endothermic fuels are liquid hydrocarbon aircraft fuels which are able to absorb the heat loads by undergoing endothermic reactions, such as thermal and catalytic cracking. The endothermic reactions are improved by catalysts which change the extent of reaction and product distribution. At high temperature, liquid hydrocarbons would lead to coke formation that can reduce the effectiveness of heat exchanger and cause rapid degradation of the catalyst, thus endothermic capacity of endothermic fuels is limited to the temperature at which coke doesn’t form. In this study, the essential cooling technologies by applying endothermic fuels and the properties of the endothermic fuels are described.

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      참고문헌 (Reference)

      1 노진현, "X-51A 스크램제트 기술 실증기 개발 프로그램 핵심 기술" 한국추진공학회 12 (12): 79-91, 2008

      2 J. Bravo, "Wall Coating of a CuO/ZnO/Al2O3 Methanol Steam Reforming Catalyst for Micro-channel Reformers" 101 : 113-121, 2004

      3 Z. Wang, "Tributylamine as an Initiator for Cracking of heptane" 49 : 1584-1594, 2008

      4 E.Corporan, "Studies of Decalin as a Suppressor of Pyrolytic Deposits in JP-8+100" AIAA 1999

      5 T.Edwards, "Propellant Requirements for Future Aerospace Propulsion Systems" AIAA 2002

      6 Z. Hai-long, "Pd/HZSM-5 Coating Catalyst for Supercritical Cracking of Endothermic Fuel" 36 (36): 462-467, 2008

      7 D. R. Sobel, "Hydrocarbon Fuel Cooling Technologies for Advanced Propulsion" 119 : 344-351, 1997

      8 A.V.Korabelnikov, "High-Temperature Conversion of Liquid Hydrocarbons" AIAA 2006

      9 H.Huang, "Fuel-Cooled Thermal Management for Advanced Aeroengines" 126 : 284-293, 2004

      10 T.Edwards, "Fuel Composition Influence on Deposition in Endothermic Fuels" AIAA 2006

      1 노진현, "X-51A 스크램제트 기술 실증기 개발 프로그램 핵심 기술" 한국추진공학회 12 (12): 79-91, 2008

      2 J. Bravo, "Wall Coating of a CuO/ZnO/Al2O3 Methanol Steam Reforming Catalyst for Micro-channel Reformers" 101 : 113-121, 2004

      3 Z. Wang, "Tributylamine as an Initiator for Cracking of heptane" 49 : 1584-1594, 2008

      4 E.Corporan, "Studies of Decalin as a Suppressor of Pyrolytic Deposits in JP-8+100" AIAA 1999

      5 T.Edwards, "Propellant Requirements for Future Aerospace Propulsion Systems" AIAA 2002

      6 Z. Hai-long, "Pd/HZSM-5 Coating Catalyst for Supercritical Cracking of Endothermic Fuel" 36 (36): 462-467, 2008

      7 D. R. Sobel, "Hydrocarbon Fuel Cooling Technologies for Advanced Propulsion" 119 : 344-351, 1997

      8 A.V.Korabelnikov, "High-Temperature Conversion of Liquid Hydrocarbons" AIAA 2006

      9 H.Huang, "Fuel-Cooled Thermal Management for Advanced Aeroengines" 126 : 284-293, 2004

      10 T.Edwards, "Fuel Composition Influence on Deposition in Endothermic Fuels" AIAA 2006

      11 M.J.Castaldi, "Development of an Effective Endothermic Fuel Platform for Regeneratively Cooled Hypersonic Vehicles" AIAA 2006

      12 O. A. Powell, "Development of Hydrocarbon-Fueled Scramjet Engines: The Hypersonic Technology(HyTech) Program" 17 (17): 1170-1176, 2001

      13 L. J. Spadaccini, "Deposit Formation and Mitigation in Aircraft Fuels" 123 : 741-746, 2001

      14 T. Edwards, "Cracking and Deposition Behavior of Supercritical Hydrocarbon Aviation Fuels" 178 : 307-334, 2006

      15 D. T. Wickham, "Additives to Improve Fuel Heat Sink Capacity in Air/Fuel Heat Exchangers" 24 (24): 55-63, 2008

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2021 평가예정 계속평가 신청대상 (등재유지)
      2018-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2015-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2011-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2009-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2006-01-01 평가 등재학술지 선정 (등재후보2차) KCI등재
      2005-02-28 학회명변경 영문명 : The Korean Society Of Propulsion Engineers -> The Korean Society of Propulsion Engineers KCI등재후보
      2005-01-01 평가 등재후보 1차 PASS (등재후보1차) KCI등재후보
      2003-01-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
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      학술지 인용정보

      학술지 인용정보
      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 0.23 0.23 0.21
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.2 0.19 0.397 0.1
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