Pressure-Coupled Responses of LOX Droplet Vaporization and Combustion in High-Pressure Hydrogen Environments

REFERENCES

• Allison, C.B., and Faeth, G.M. 1975. Open-loop response of a burning liquid monopropellant. AIAA J., 13, 1287–1294.
   Google Scholar
• Bathia, R., and Sirignano, W.A. 1991. One-dimensional analysis of liquid-fueled combustion instability. J. Propul. Power, 7, 953–961.
   Web of Science ®Google Scholar
• Burke, M.P., Chaos, M., Ju, Y., Dryer, F.L., and Klippenstein, S.J. 2012. Comprehensive H2/O2 kinetic model for high-pressure combustion. Int. J. Chem. Kinet., 44, 444–474.
   Web of Science ®Google Scholar
• Cheroudi, B., Talley, D., and Coy, E. 2002. Visual characteristics and initial growth rate of round cryogenic jets at subcritical and supercritical pressures. Phys. Fluids, 14, 850–861.
   Web of Science ®Google Scholar
• Culick, F.E.C., and Yang, V. 1995. Overview of combustion instabilities in liquid-propellant rocket engines. In V. Yang and W.E. Anderson ( Eds.), Liquid Rocket Engine Combustion Instability, Vol. 169, Progress in Astronautics and Aeronautics, American Institute of Aeronautics and Astronautics, Washington, DC, pp. 3–37.
   Google Scholar
• Curtis, E.W., and Farrel, P.V. 1992. A numerical study of high pressure vaporization. Combust. Flame, 90, 85–102.
   Web of Science ®Google Scholar
• Daou, J., Haldenwang, P., and Nicoli, C. 1995. Supercritical burning of liquid (LOX) droplet with detailed chemistry. Combust. Flame, 101, 153–169.
   Web of Science ®Google Scholar
• Delplanque, J.P., and Sirignano, W.A. 1993. Numerical study of the transient vaporization of an oxygen droplet at sub- and super-critical conditions. Int. J. Heat Mass Transfer, 36, 303–314.
   Web of Science ®Google Scholar
• Delplanque, J.P., and Sirignano, W.A. 1996. Transcritical liquid oxygen droplet vaporization: Effect on rocket combustion instability. J. Propul. Power, 12, 349–357.
   Web of Science ®Google Scholar
• Harstad, K., and Bellan, J. 1998. Isolated fluid oxygen drop behavior in fluid hydrogen at rocket chamber pressures. Int. J. Heat Mass Transfer, 41, 3537–3550.
   Web of Science ®Google Scholar
• Heidmann, M.F., and Wieber, P.R. 1966. Analysis of frequency response characteristics of propellant vaporization. Technical Report, NASA TN D3749.
   Google Scholar
• Hsiao, G.C., Meng, H., and Yang, V. 2011. Pressure-coupled vaporization response of n-pentane fuel droplet at subcritical and supercritical conditions. Proc. Combust. Inst., 33, 1997–2003
   Web of Science ®Google Scholar
• Hsieh, K.C., Shuen, J.S., and Yang, V. 1991. Droplet vaporization in high-pressure environments I: Near critical conditions. Combust. Sci. Technol., 76, 111–132.
   Web of Science ®Google Scholar
• Hua, Y.-X., Wang, Y.-Z., and Meng, H. 2010. A numerical study of supercritical forced convective heat transfer of n-heptane inside a horizontal miniature tube. J. Supercrit. Fluids, 52, 36–46
   Web of Science ®Google Scholar
• Lafon, P., Meng, H., Yang, V., and Habiballah, M. 2008. Vaporization of liquid oxygen (LOX) droplets in hydrogen and water environments under sub- and super-critical conditions. Combust. Sci. Technol., 180, 1–26.
   Web of Science ®Google Scholar
• Lieuwen, T.C., and Yang, V. ( Eds.) 2005. Combustion Instabilities in Gas Turbine Engines: Operational Experience, Fundamental Mechanisms, and Modeling, Vol. 210, Progress in Astronautics and Aeronautics, American Institute of Aeronautics and Astronautics, Washington, DC.
   Google Scholar
• Masoudi, M., and Sirignano, W.A. 2000. Collision of a vortex with a vaporizing droplet. Int. J. Multiphase Flow, 26, 1925–1949.
   Web of Science ®Google Scholar
• Meng, H., Hsiao, G.C., Yang, V., and Shuen, J.S. 2005. Transport and dynamics of liquid oxygen droplets in supercritical hydrogen streams. J. Fluid Mech., 527, 115–139.
   Web of Science ®Google Scholar
• Meng, H., and Yang, V. 2003. A unified treatment of general fluid thermodynamics and its application to a preconditioning scheme. J. Comput. Phys., 189, 277–304.
   Web of Science ®Google Scholar
• Meng, H., and Yang, V. 2012. Clustering effects on liquid oxygen (LOX) droplet vaporization in hydrogen environments at subcritical and supercritical pressures. Int. J. Hydrogen Energy, 37, 11815–11823.
   Web of Science ®Google Scholar
• Meng, H., and Yang, V. 2014. Vaporization of two liquid oxygen (LOX) droplets in tandem in convective hydrogen streams at supercritical pressures. Int. J. Heat Mass Transfer, 68, 500–508.
   Web of Science ®Google Scholar
• Oschwald, M., Smith, J.J., Branam, R., Hussong, J., Shick, A., Cheroudi, B., and Talley, D. 2006. Injection of fluids into supercritical environments. Combust. Sci. Technol., 178, 49–100.
   Web of Science ®Google Scholar
• Roy, A., and Segal, C. 2010. Experimental study of fluid jet mixing at supercritical conditions. J. Propul. Power, 26, 1205–1211.
   Web of Science ®Google Scholar
• Schmitt, T., Rodriguez, J., Leyva, I.A., and Candel, S. 2012. Experimental and numerical simulation of mixing under supercritical conditions. Phys. Fluids, 24, 055104.
   Web of Science ®Google Scholar
• Shuen, J.S., Yang, V., and Hsiao, G.C. 1992. Combustion of liquid-fuel droplet in supercritical conditions. Combust. Flame, 89, 299–319.
   Web of Science ®Google Scholar
• Sirignano, W.A., and Delplanque, J.P. 1999. Transcritical vaporization of liquid fuels and propellants. J. Propul. Power, 15, 896–902.
   Web of Science ®Google Scholar
• Sirignano, W.A., Delplanque, J.P., Chiang, C.H., and Bhatia, H. 1995. Liquid-propellant droplet vaporization: A rate-controlling process for combustion instability. In V. Yang and W.E. Anderson ( Eds.), Liquid Rocket Engine Combustion Instability, Vol. 169, Progress in Astronautics and Aeronautics, American Institute of Aeronautics and Astronautics, Washington, DC, pp. 307–343.
   Google Scholar
• Strahle, W.C. 1965. Periodic solutions to a convective droplet burning problem: The stagnation point. Proc. Combust. Inst., 10, 1315–1325.
   Google Scholar
• Tong, A.Y., and Sirignano, W.A. 1989. Oscillatory vaporization of fuel droplets in an unstable combustor. J. Propul. Power, 5, 257–261.
   Web of Science ®Google Scholar
• Wang, Y.-Z., Hua, Y.-X., and Meng, H. 2010. Numerical study of supercritical turbulent convective heat transfer of cryogenic-propellant methane. J. Thermophys. Heat Transfer, 24, 490–500.
   Web of Science ®Google Scholar
• Wicker, J.M., Greene, W.D., Kim, S.I., and Yang, V. 1996. Triggering of longitudinal combustion instabilities in rocket motors: Nonlinear combustion response. J. Propul. Power, 6, 1148–1158.
   Web of Science ®Google Scholar
• Yan, C., and Aggarwal, S.K. 2006. A high-pressure droplet model for spray simulations. J. Eng. Gas Turbines Power, 128, 482–492.
   Web of Science ®Google Scholar
• Yang, V. 2000. Modeling of supercritical vaporization, mixing, and combustion processes in liquid-fueled propulsion systems. Proc. Combust. Inst., 28, 925–942.
   Web of Science ®Google Scholar
• Yang, V., and Anderson, W.E. ( Eds.) 1995. Liquid Rocket Engine Combustion Instability, Vol. 169, Progress in Astronautics and Aeronautics, American Institute of Aeronautics and Astronautics, Washington, DC.
   Google Scholar
• Yang, V., Lin, N.N., and Shuen, J.S. 1994. Vaporization of liquid oxygen (LOX) droplets in supercritical hydrogen environments. Combust. Sci. Technol., 97, 247–270.
   Web of Science ®Google Scholar
• Zhu, G.S., and Reitz, R.D. 2002. A model for high-pressure vaporization of droplets of complex mixtures using continuous thermodynamics. Int. J. Heat Mass Transf., 45, 495–507.
   Web of Science ®Google Scholar
• Zong, N., Meng, H., Hiesh, S.-Y., and Yang, V. 2004. A numerical study of cryogenic fluid injection and mixing under supercritical conditions. Phys. Fluids, 16, 4248–4261.
   Web of Science ®Google Scholar
• Zong, N., and Yang, V. 2006. Cryogenic fluid jets and mixing layers in transcritical and supercritical environments. Combust. Sci. Technol., 178, 193–227.
   Web of Science ®Google Scholar