한국항공우주학회지 (Journal of the Korean Society for Aeronautical & Space Sciences)

  • 제38권8호
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  • Pages.823-833
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  • 2010
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  • 1225-1348(pISSN)
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  • 2287-6871(eISSN)
한국항공우주학회 (The Korean Society for Aeronautical and Space Sciences)
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초임계 영역에서 대체 모델 연료를 이용한 케로신의 열역학적 상태량 연구

Investigation of Thermophysical Properties of the Kerosene Using the Surrogate Model Fuel at Supercritical Conditions

  • 김국진 (한국항공대학교 항공우주및기계공학과) ;
  • 허준영 (한국항공대학교 항공우주및기계공학과) ;
  • 성홍계 (한국항공대학교 항공우주및기계공학부)
  • 투고 : 2010.04.07
  • 심사 : 2010.06.01
  • 발행 : 2010.08.01
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초록

액체 로켓 및 항공용 엔진 연료로서 사용되는 케로신의 열역학적 상태량을 연구하기 위해 surrogate 모델이 조사되었다. 초임계 조건에서 실제 기체 상태 방정식(SRK 상태 방정식, PR 상태 방정식)과 NIST SUPERTRAPP(ECS 원리)을 이용하였을 경우의 밀도 분포가 기존의 실험 결과와 비교되었다. 또한 surrogate 모델의 종류에 따른 열역학적 상태량의 오차 범위에 대한 고찰이 수행되었다. 탄화 수소 계열 연료에 대해서는 PR 상태 방정식과 ECS 원리가 높은 정확도를 나타내지만 압력, 온도와 같은 작동 환경에 따라 적절한 surrogate 모델을 선별하여 선택해야 함을 확인하였다.

For the study of thermophysical properties of kerosene for the liquid rocket and aviation fuels, the surrogate models are investigated. The density distributions based on the real gas equations of state(Soave modification of Redlich-Kwong and Peng-Robinson equation of state) and NIST SUPERTRAPP(extended corresponding state principle) are compared with the previous experimental results at supercritical conditions. The error range of thermophysical properties analyzed for the surrogate models as well. Peng-Robinson equation of state and extended corresponding state principle are especially accurate for the hydrocarbon fuels but the appropriate surrogate models need to be chosen to the operation conditions such as pressure and temperature.

키워드

과제정보

연구 과제 주관 기관 : 한국 연구 재단

참고문헌

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피인용 문헌

  1. Study on Thermophysical Property Characteristics of a 4 Species Kerosene Surrogate in a Swirl Injector at Supercritical Pressure Condition vol.17, pp.6, 2013, https://doi.org/10.6108/KSPE.2013.17.6.048