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http://dx.doi.org/10.5139/JKSAS.2010.38.8.823

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

Kim, Kuk-Jin (한국항공대학교 항공우주및기계공학과)
Heo, Jun-Young (한국항공대학교 항공우주및기계공학과)
Sung, Hong-Gye (한국항공대학교 항공우주및기계공학부)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.38, no.8, 2010 , pp. 823-833 More about this Journal
Abstract
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.
Keywords
Kerosene; Surrogate Model; Supercritical Conditions; Real Gas Equation of State; Thermophysical Property;
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Times Cited By KSCI : 1  (Citation Analysis)
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1 Burkhardt, H., Sippel, M., Herbertz, A., and Klevanski, J., "Kerosene vs Methane: A Propellant Tradeoff for Reusable Liquid Booster Stages", Journal of Spacecraft and Rockets, Vol. 41, No. 5, 2004, pp. 762-769.   DOI   ScienceOn
2 Annamalai, K., and Puri, I. K., Advanced Thermodynamics Engineering, Imported Ed., CRC Press, Boca Raton, 2002, pp. 296-298.
3 Poling, B. E., Prausnitz, J. M., and O'Connell, J. P., The Properties of Gases and Liquids, 5th Ed., McGraw-Hill, New York, 2001, pp. 2.23-2.26.
4 Sengers, J. V., Kayser, R. F., Peters, C. J., and White, H. J., Jr., Equations of State for Fluids and Fluid Mixtures, 1st Ed., Part I, IUPAC, Amsterdam, 2000, pp. 76-86.
5 Ely, J. F. and Hanley, J. M., "Prediction of Transport Properties. !. Viscosity of Fluids and Mixtures", Industrial and Engineering Chemistry Fundamentals, Vol. 20, No. 4, 1981, pp. 323-332.   DOI
6 Ely, J. F. and Hanley, J. M., "Prediction of Transport Properties. 2. Thermal Conductivity of Pure Fluids and Mixtures", Industrial and Engineering Chemistry Fundamentals, Vol. 22, No. 1, 1983, pp. 90-97.   DOI
7 Yang, J. C., Vazquez, I., Boyer, C. I., Huber, M. L., and Weber, L., "Measured and Predicted Thermodynamic Properties of Selected Halon Alternative/Nitrogen Mixtures", International Journal of Refrigeration, Vol. 20, No. 2, 1997, pp. 96-105.   DOI   ScienceOn
8 Huber, M. L., "NIST Standard Reference Database 4 - NIST Thermophysical Properties of Hydrocarbon Mixtures Database (SUPERTRAPP) Version 3.2 Users' Guide", National Institute of Standards and Technology, January 2007, Gaithersburg, Maryland.
9 Yu, G., Li, J. G., Zhao, Z., Chang, X. Y., and Sung, C. J., "Investigation of Vaporized Kerosene Injection in a Supersonic Model Combustor", AIAA Paper No. 2003-6938, 12th AIAA International Space Planes and Hypersonic Systems and Technologies, 15-19 December 2003, Norfolk, Virginia.
10 Yu, G., Fan, X. J., Li, J. G., Yue, L. J., Zhang, X. Y., and Sung, C. J., "Characterization of a Supersonic Model Combustor with Partially-Cracked Kerosene", AIAA Paper No. 2005-3714, 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 10-13 July 2005, Tucson, Arizona.
11 Shafer, L. M., Striebich, R. C., Gomach, J., and Edwards, T., "Chemical Class Composition of Commercial Jet Fuels and Other Specialty Kerosene Fuels", AIAA Paper No. 2006-7972, 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 6-9 November 2006, Canberra, Australia.
12 Magee, J. W., Bruno, T. J., Friend, D. G., Huber, M. L., Laesecke, A., Lemmon, E. W., McLinden, M. O., Perkins, R. A., Baranski, J., and Widegren, J. A., "Thermophysical Properties Measurements and Models for Rocket Propellant RP-1: Phase I", NISTIR 6646, 2007.
13 Montgomery, C. J., Cannon, S. M., Mawid, M. A., and Sekar, B., "Reduced Chemical Kinetic Mechanisms for JP-8 Combustion", AIAA Paper No. 2002-0336, 40th AIAA Aerospace Sciences Meeting and Exhibit, 14-17 January 2002, Reno, Nevada.
14 Fan, X. J., Yu, G., Li, J. G., Zhang, X. Y., and Sung, C. J., "Investigation of Vaporized Kerosene Injection and Combustion in a Supersonic Model Combustor", Journal of Propulsion and Power, Vol. 22, No. 1, 2006, pp. 103-110.   DOI   ScienceOn
15 Tucker, K. C., "A Flash Vaporization System for Detonation of Hydrocarbon Fuels in a Pulse Detonation Engine", Ph. D Dissertation, Air Force Institute of Technology, 2005.
16 Miser, C. L., Helfrich, T. M., Phelps, D. K., and Schauer, F. R., "Supercritical Fuel Density from an Experimental Pulsed Detonation Engine", AIAA Paper No. 2006-1025, 44th AIAA Aerospace Sciences Meeting and Exhibit, 9-12 January 2006, Reno, Nevada.
17 김국진, 허준영, 김종찬, 구자예, 성홍계, "초임계 영역에서 실제 기체 상태 방정식에 따른 단일 성분의 열역학적 상태량 비교 연구", 한국추진공학회지, 제 14권, 제 3호, 2010, pp. 39-51.
18 Wang, T. S., "Thermo-Kinetics Characterization of Kerosene/RP-1 Combustion", AIAA Paper No. 1996-2887, 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 1-13 July 1996, Lake Buena Vista, Florida.
19 Huang, H., Sobel, D. R., and Spadaccini, L. J., "Endothermic Heat-Sink of Hydrocarbon Fuels for Scramjet Cooling", AIAA Paper No. 2002-3871, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 7-10 July 2002, Indianapolis, Indiana.
20 Edwards, T., ""Kerosene" Fuels for Aerospace Propulsion - Composition and Properties", AIAA Paper No. 2002-3874, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 7-10 July 2002, Indianapolis, Indiana.