Huang H, Spadaccini L. J., Dobel D. R. Fuel-cooled thermal management for advanced aero engines[C]. Proceedings of ASME Turbo Expo 2002. Amsterdam, Holland: ASME, GT-2002-30070.
[2]
Wu P K, Chen T H. Injection of supercritical ethylene in nitrogen[R]. AIAA 95-0382, 1995
[3]
Wu P K, Shahnam M, Kirken dall K. Expansion and mixing processes of underexpanded supercritical fuel jets injection into superheated conditions[R]. AIAA 97-2852.
[4]
Chehroudi B, Talley D, and Coy E. Visual characteristics and initial growth rates of round cryogenic jets at subcritical and supercritical pressures[J]. Phy. Fluids. 2002,14: 850-861
[5]
Barata J, Gokalp I, and Silva A. Numerical study of cryogenic jets under supercritical conditions[J]. J. Prop. Power. 2003,19:142-147.
[6]
Chen L D, Sui P C. Atomization during the injection of supercritical fluid into high-pressure environment[C]. 1994 IUTAM on Droplets and Sprays, Taiwan, Dec 1994. Industrial and Chemical Engineering Research.
[7]
Chen L. Heat transfer, fouling and combustion of supercritical fuels[R]. Def. Tech. Info. Center, Report#940321.
[8]
Douthip T, Ervin J, Williams T, and Bento J. Studies of injection of jet fuel at supercritical conditions[J]. Ind. Eng. Chem. Res., 2002, 41: 5856-5866.
[9]
Minotti A, Bruno C. Comparison between real and ideal sub and supercritical combustion simulations of LO2-CH4 LRE flames at 15MPa[C]. 46th AIAA Aerospace sciences meeting and exhibit, AIAA2008-951, 1997.
[10]
Peng D Y, Robinson D B. A new two-constant equation of state[J]. Ind. Eng. Chem. Fundam., 1976, 15:59.
[11]
Reid R C, John M P, and Bruce E P. The prosperities of gases and liquids[M]. McGraw Hill International Editions, 4th Ed. Chap1-5, 8-11, Singapore, 1989.
[12]
Congiunti A, Bruno C, and Ciacomazzi E. Supercritical combustion properties[C]. 41st Aerospace sciences meeting and exhibit. AIAA2003-478, 2003.
[13]
Chung T H, Ajlan M, and Lee K E. Generalized multiparameter corresponding state correlation for polyatomic, polar fluid transport prosperities[J]. Industrial and Chemical Engineering Research. 1988, 77: 671-679.
[14]
Edwards T, Maurice L Q. Surrogate mixtures to represent complex aviation and rocket fuels[J]. J. Prop. Power. 2001,17:461.
[15]
Weiss J M, Smith W A. Preconditioning applied to variable and constant density flows[J]. AIAA J. 1995, 33:2050-2057.