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Numerical study of the pseudo-boiling phenomenon in the transcritical liquid oxygen/gaseous hydrogen flame

Zeinivand, H ; Sharif University of Technology | 2020

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  1. Type of Document: Article
  2. DOI: 10.1177/0954410020964692
  3. Publisher: SAGE Publications Ltd , 2020
  4. Abstract:
  5. The interactions and effects of turbulent mixing, pseudo-boiling phenomena, and chemical reaction heat release on the combustion of cryogenic liquid oxygen and gaseous hydrogen under supercritical pressure conditions are investigated using RANS simulations. Comparisons of the present numerical simulation results with available experimental data reveal a reasonably good prediction of a supercritical axial shear hydrogen-oxygen flame using the standard k-ε turbulence model and the eddy dissipation concept combustion model with a 23 reaction steps kinetics for H2-O2 reaction. The present simulation qualitatively reproduced oxygen injection and its reaction with the co-flowing hydrogen, which is characterized by rapid flame expansion, downstream flame propagation, and expansion induced flow recirculation. Several turbulence models were used for numerical simulations. It is shown that the selection of an appropriate turbulence model for transcritical reacting flows is crucial and far more important than for subcritical reacting flows. It is indicated that the pseudo-boiling phenomena is the main reason for the considerable differences between the turbulence models in a transcritical flame. Also, it is demonstrated that the liquid oxygen core disappears faster in a non-reacting flow than in a reacting flow. The shear layer in the non-reacting flow is much stronger than reacting case; providing a large transfer of energy from the outer layer to the inner layer. At the supercritical injection conditions, the difference between the turbulence models is much less than the transcritical injection conditions. © IMechE 2020
  6. Keywords:
  7. Cryogenic propellants ; Pseudo-boiling ; Supercritical combustion ; Transcritical injection ; Energy transfer ; Expansion ; Hydrogen ; Liquefied gases ; Numerical models ; Oxygen ; Reaction kinetics ; Shear flow ; Turbulence models ; Combustion model ; Eddy dissipation concept ; Flame propagation ; Gaseous hydrogen ; Hydrogen-oxygen flame ; Injection conditions ; Standard k epsilons ; Super-critical pressures ; Combustion
  8. Source: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering ; 2020
  9. URL: https://journals.sagepub.com/doi/abs/10.1177/0954410020964692