Miniature Supersonic Burner for the Study of Combustion at Extreme Conditions. II: External Flow
Publication: Journal of Energy Engineering
Volume 144, Issue 5
Abstract
A miniature supersonic burner has been designed with the purpose of studying extreme flow-chemistry interaction. The system combines a first-stage, lean premixed methane/air burner that creates a vitiated flow at pressure and a second-stage burner where additional fuel (methane) is added to the flow before exiting the system through a converging nozzle. In this part, a one-dimensional (1D) detailed chemistry calculation of the reacting flow at the exit of the jet is conducted. The mixture of gases is allowed to expand isentropically to the conditions expected at the exit of the supersonic jet. The viscous and conducting flow field through a shock wave is calculated using the GRI3.0 kinetic scheme. The structure of the standing detonation downstream of the Mach stem is examined for different initial concentrations of hydrogen atoms. Results point to the extreme suppression of chemistry through the supersonic flow field and the creation of low Damköhler numbers in the exit of the miniature burner.
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Acknowledgments
NSF support through Grant No. 0933633 Song-Charng Kong, program manager) is gratefully acknowledged. The author wishes to recognize contributions by Wenjiang Xu during the early stages of this work.
References
Addy, A. L. 1981. “Effects of axisymmetric sonic nozzle geometry on Mach disk characteristics.” AIAA J. 19 (1): 121–122. https://doi.org/10.2514/3.7751.
Barlow, R. S., H. C. Ozarovsky, A. N. Karpetis, and R. P. Lindstedt. 2009. “Piloted jet flames of CH4/H2/air: Experiments on localized extinction in the near field at high Reynolds numbers.” Combust. Flame 156 (11): 2117–2128. https://doi.org/10.1016/j.combustflame.2009.04.005.
Bayeh, A. 2013. “Rotational and vibration Raman spectroscopy for thermochemistry measurements in supersonic flames.” Ph.D. thesis, Texas A&M Univ.
Bayeh, A. C., D. W. Ellis, and A. N. Karpetis. 2014. “Miniaturized combustor for supersonic methane-air flames.” J. Propul. Power 30 (5): 1167–1174. https://doi.org/10.2514/1.B34841.
Brinkley, S., and L. Seely. 1969. “Construction of the Hugoniot curve and calculation of the Chapman-Jouguet points for general equations of state.” Combust. Flame 13 (5): 506–510. https://doi.org/10.1016/0010-2180(69)90090-X.
Brown, P., G. Byrne, and A. Hindmarsh. 1989. “VODE—A variable-coefficient ODE solver.” SIAM J. Sci. Stat. Comput. 10 (5): 1038–1051. https://doi.org/10.1137/0910062.
Browne, S., J. Ziegler, and J. E. Shepherd. 2015. Numerical solution methods for shock and detonation jump conditions. Pasadena, CA: California Institute of Technology.
Burke, U., K. P. Somers, P. O’Toolea, C. M. Zinner, N. Marquet, G. Bourque, E. L. Petersen, W. K. Metcalfe, Z. Serinyel, and H. J. Curran. 2015. “An ignition delay and kinetic modeling study of methane, dimethyl ether, and their mixtures at high pressures.” Combust. Flame 162 (2): 315–330. https://doi.org/10.1016/j.combustflame.2014.08.014.
Chao, J., H. Ng, and J. Lee. 2009. “Detonability limits in thin annular channels.” Proc. Combust. Inst. 32 (2): 2349–2354. https://doi.org/10.1016/j.proci.2008.05.090.
Curtiss, C., J. Hirschfelder, and M. Barnett. 1959. “Theory of detonations. III: Ignition temperature approximation.” J. Chem. Phys. 30 (2): 470–492. https://doi.org/10.1063/1.1729976.
Doering, W. 1943. “Über den Detonationsvorgang in Gasen.” Annalen der Physik 435 (6–7): 421–436. https://doi.org/10.1002/andp.19434350605.
Erpenbeck, J. 1962. “Stability of steady state equilibrium detonations.” Phys. Fluids 5 (5): 604–614. https://doi.org/10.1063/1.1706664.
Fickett, W., and W. Davis. 1979. Detonation. Berkeley, CA: University of California Press.
Glassman, I. 2008. Combustion. 4th ed. Boston: Academic Press.
Goodwin, D. 2003. “An open-source, extensible software suite for CVD process simulation.” Chem. Vapor Deposition XVI EUROCVD 14 (40): 2003–2008.
Hatanaka, K., and T. Saito. 2012. “Influence of nozzle geometry on underexpanded axisymmetric free jet characteristics.” Shock Waves 22 (5): 427–434. https://doi.org/10.1007/s00193-012-0391-x.
Hirschfelder, J., and C. Curtiss. 1958. “Theory of detonations. I: Irreversible unimolecular reaction.” J. Chem. Phys. 28 (6): 1130–1147. https://doi.org/10.1063/1.1744357.
Hirschfelder, J., C. Curtiss, and R. Bird. 1954. Molecular theory of gases and liquids. New York: Wiley.
Karpetis, A., D. Ellis, and A. Bayeh. 2018. “A miniature supersonic burner for the study of combustion at extreme conditions. Part I: Internal flow.” Energy Eng. J. 144 (5): 04018057. https://doi.org/10.1061/(ASCE)EY.1943-7897.0000573.
Lee, J. 1984. “Dynamic parameters of gaseous detonations.” Ann. Rev. Fluid Mech. 16 (1): 311–336. https://doi.org/10.1146/annurev.fl.16.010184.001523.
Li, C., K. Kailasanath, and E. Oran. 1994. “Detonation structures behind oblique shocks.” Phys. Fluids 6 (4) : 1600–1614. https://doi.org/10.1063/1.868273.
Liepmann, H., and A. Roshko. 1957. Elements of gas dynamics. New York: Wiley.
Linder, B., C. Curtiss, and J. Hirschfelder. 1958. “Theory of detonations. II. Reversible unimolecular reaction.” J. Chem. Phys. 28 (6): 1147–1151. https://doi.org/10.1063/1.1744358.
Lindstedt, R. P., H. C. Ozarovsky, R. S. Barlow, and A. N. Karpetis. 2007. “Progression of localized extinction in high Reynolds number turbulent jet flames.” Proc. Combust. Inst. 31 (1): 1551–1558. https://doi.org/10.1016/j.proci.2006.08.099.
Matsuo, S., M. Tanaka, Y. Otobe, H. Kashimura, H.-D. Kim, and T. Setoguchi. 2004. “Effect of axisymmetric sonic nozzle geometry on characteristics of supersonic air jet.” J. Therm. Sci. 13 (2): 121–126. https://doi.org/10.1007/s11630-004-0019-2.
Nakamura, T. 2010. “Computational analysis of Zeldovich-von Neumann-Doering (ZND) detonation.” M.S. thesis, Texas A&M Univ.
Otobe, Y., H. Kashimura, S. Matsuo, T. Setoguchi, and H.-D. Kim. 2008. “Influence of nozzle geometry on the near-field structure of a highly underexpanded sonic jet.” J. Fluids Struct. 24 (2): 281–293. https://doi.org/10.1016/j.jfluidstructs.2007.07.003.
Romick, C., T. Aslam, and J. Powers. 2012. “The effect of diffusion on the dynamics of unsteady detonations.” J. Fluid Mech. 699 (1) : 453–464. https://doi.org/10.1017/jfm.2012.121.
Shepherd, J. 1986. “Chemical kinetics of hydrogen-air-diluent detonations.” Prog. Astronautics Aeronaut. 106: 263–293. https://doi.org/10.2514/5.9781600865800.0263.0293.
Smith, G. P., et al. 2000. “The GRI 3.0 chemical mechanism.” Accessed November 23, 2017. http://www.me.berkeley.edu/gri_mech/.
Vincenti, W. G., and C. H. Kruger. 1965. Introduction to physical gas dynamics. New York: Wiley.
von Neumann, J. 1963. Theory of detonation waves. New York: Pergamon Press.
Williams, F. 1985. Combustion theory. 2nd ed. Redwood City, CA: Addison-Wesley.
Zel'dovich, Y. 1950. On the theory of the propagation of detonation in gaseous systems. Washington, DC: National Advisory Committee for Aeronautics.
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©2018 American Society of Civil Engineers.
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Received: Feb 10, 2018
Accepted: May 8, 2018
Published online: Aug 10, 2018
Published in print: Oct 1, 2018
Discussion open until: Jan 10, 2019
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