한국분무공학회지 (Journal of ILASS-Korea)

  • 제26권4호
  • /
  • Pages.171-181
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  • 2021
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  • 1226-2277(pISSN)
  • /
  • 2288-9051(eISSN)
한국분무공학회 (Institute for Liquid Atomization and Spray Systems-Korea)
권호 표지
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초임계 탄화수소 항공유의 열역학적 물성치 예측 기법 연구

Investigation on a Prediction Methodology of Thermodynamic Properties of Supercritical Hydrocarbon Aviation Fuels

  • 황성록 (부경대학교 대학원 기계공학과) ;
  • 이형주 (부경대학교 기계공학과)
  • 투고 : 2021.08.31
  • 심사 : 2021.09.29
  • 발행 : 2021.12.31
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초록

This study presents a prediction methodology of thermodynamic properties by using RK-PR Equation of State in a wide range of temperature and pressure conditions including both sub-critical and super-critical regions, in order to obtain thermophysical properties for hydrocarbon aviation fuels and their products resulting from endothermic reactions. The density and the constant pressure specific heat are predicted in the temperature range from 300 to 1000 K and the pressure from 0.1 to 5.0 MPa, which includes all of the liquid and gas phases and the super-critical region of three representative hydrocarbon fuels, and then compared with those data obtained from the NIST database. Results show that the averaged relative deviations of both predicted density and constant pressure specific heat are below 5% in the specified temperature and pressure conditions, and the major sources of the errors are observed near the saturation line and the critical point of each fuel.

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과제정보

본 연구는 2020년도 2학기 부경대학교 신임교수 학술연구지원사업으로 수행되었습니다(과제번호 : CD20201539).

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