한국추진공학회지 (Journal of the Korean Society of Propulsion Engineers)

  • 제17권4호
  • /
  • Pages.73-80
  • /
  • 2013
  • /
  • 1226-6027(pISSN)
  • /
  • 2288-4548(eISSN)
한국추진공학회 (The Korean Society of Propulsion Engineers)
권호 표지
DOI QR코드

DOI QR Code

흡열연료를 이용한 연료분사 및 연소 특성 연구동향

Research Activities about Characteristics of Fuel Injection and Combustion Using Endothermic Fuel

  • Choi, Hojin (4-Advanced Propulsion Technology center, Agency foe Defence Development) ;
  • Lee, Hyungju (4-Advanced Propulsion Technology center, Agency foe Defence Development) ;
  • Hwang, Kiyoung (4-Advanced Propulsion Technology center, Agency foe Defence Development)
  • 투고 : 2012.11.30
  • 심사 : 2013.04.11
  • 발행 : 2013.08.01
PDF 다운로드
⟨ 이전 논문 다음 논문 ⟩

초록

장거리 극초음속 비행체에 적용 가능한 유일한 냉각방안으로 알려져 있는 흡열연료 적용기술을 개발하기 위하여 흡열반응에 의해 분해된 연료의 분사 및 연소특성에 대한 연구사례를 살펴보았다. 흡열반응을 거친 연료가 연소실에 분사될 때 처해지는 초임계 상태의 분사 특성, 초임계 연료가 초음속 유동장에 분사될 때의 공기혼합 특성 등에 관한 연구사례를 살펴보았고, 연소특성으로서 점화지연시간 및 화염전파 속도에 미치는 영향, 초음속 연소실에서 연소될 때의 연소효율 상승 연구사례 등을 살펴보았다. 국내에서 수행된 흡열연료 관련 연구동향을 살펴보았다.

Endothermic fuel utilizing technology is considered as a unique practical method of hypersonic vehicle for long distance flight. Research activities about characteristics of fuel injection and combustion using cracked by endothermic reaction are reviewed. Studies on characterization of supercritical fuel injection and mixing within supersonic flow field are surveyed. Researches on combustion characteristics such as ignition delay time, laminar burning velocity and combustion efficiency at supersonic model combustor are reviewed. In addition, domestic research activities on endothermic fuel are surveyed.

키워드

참고문헌

  1. Edwards, T., "UASF supercritical hydrocarbon fuels interests," 31st Aerospace Sciences Meeting, Reno, NV, U.S.A, AIAA-93-0807, 1993.
  2. Ianovsky, L. S., Sosounov, V. A., and Shikhman, Y. M., "Endothermic Fuels for Hypersonic Aviation," AGARD CP-536, pp. 44-1, 44-8, 1993.
  3. Edwards, T. and Maurice, L., "HYTECH fuels/fuel system research," 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Norfolk,VA,U.S.A., AIAA-98-1562, 1998.
  4. Crook, Loren C., Rachedi, Robert R. and Sojka, Paul E., "Development of a Real-Fuel Supercritical Injection Facility," 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cincinnati, OH, U.S.A, AIAA 2007-5683, 2007.
  5. Wu, P., Chen, T.H., Nejad, A.S., Carter, C.D., "Injection of Supercritical Ethylene in Nitrogen," Journal of Propulsion and Power, Vol. 12, No. 4, pp. 770-777, 1996. https://doi.org/10.2514/3.24100
  6. Chehroudi, B., Talley, D. and Coy, E., "Initial Growth Rate and Visual Characteristics of Round Jet into a Sub- to Supercritical Environment of Relevance to Rocket, Gas Turbine, and Diesel Engines," 37th Aerospace Sciences Meeting and Exhibit, Reno, NV, U.S.A, AIAA-99-0206, 1999.
  7. Gao, W. Liang, H.S., Xu, Q.. Lin, Y.Z. and Sung, C.J., "Injection of Supercritical Aviation kerosene fuel into quiescent atmospheric environment," 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Denver, Colorado, U.S.A, AIAA2009-4927, 2009.
  8. Chen, L.D. and Sui, P.C., "Atomization During the Injection of Supercritical Fluid into High-Pressure Environment," 1994 IUTAM on Droplets and Sprays, 1994.
  9. Hermanson, T.C., Papas, P. and Kay, I.W., "Structure and Penetration of a Transverse Fluid Jet Injected at Supercritical Pressure into Supersonic Flow," 28th Joint Propulsion Conference and Exhibit, Nashville,TN,U.S.A., AIAA 92-3652, 1992.
  10. Fan, X.J., Yu, G., Li, J.G., Zhang, X.Y. and Sung, C.J., "Injection and Combustion of Vaporized Kerosene in a Supersonic Model Combustor," Journal of Propulsion and Power, Vol. 22, No. 1, pp. 103-110, 2006. https://doi.org/10.2514/1.15427
  11. Colket, M.B., III, and Spadaccini, L.J., "Scramjet Fuels Autoignition Study," Journal of Propulsion and Power, Vol. 17, No. 2, pp. 315-323, 2001. https://doi.org/10.2514/2.5744
  12. Ji, C., You, X., Holley, A.T., Wang, Y.L., Egolfopoulos, F.N. and Wang, H., "Propagation and Extinction of Mixtures of Air with n-Dodecane, JP-7, and JP-8 Jet Fuels," 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, U.S.A, AIAA 2008-974, 2008.
  13. Axel VINCENT-RANDONNIER, Bruno ROUXEL, et al, "Experimental investigations on the self-ignition of a thermally decomposed endothermic fuel in hot supersonic air flow in the MPP-LAERTE combustion test bench," 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, Ohio, U.S.A, AIAA2008-2676, 2008.
  14. Fan, X.J., Yu, G., Li, J.G., Zhang, X.Y. and Sung, C.J., "Combustion and Ignition of thermally cracked kerosene in supersonic model combustors," Journal of Propulsion an d Power, Vol. 23, No. 2, pp. 317-324, 2007. https://doi.org/10.2514/1.26402