Direct numerical simulation of gas-surface interactions within a turbulent reacting hypersonic boundary layer

POSTER

Abstract



Viscous dissipation in high-Mach hypersonic boundary layers activates non-equilibrium thermochemical processes in the form of internal-energy excitation and dissociation/recombination phenomena. With the characteristic rates of gas-phase chemical reactions comparable to those of integral-scale turbulent fluctuations, the chemical production rates of radical species are significantly modulated by turbulent mixing of thermodynamic states in hypersonic boundary layers. In this work, we present direct numerical simulation results for a high-temperature turbulent boundary layer overriding an ablative boundary with oxidation, nitridation, and sublimation surface reactions. Statistical analysis of turbulence/chemistry interaction is presented for both surface chemistry and gas-phase processes involving ablation products. Analysis of reaction-rate closure modeling for coarse-grained computations is conducted a priori, with a particular emphasis on representations for subfilter reactive processes in the context of large-eddy simulation.

Presenters

  • Christopher Thomas Williams

    Center for Turbulence Research, Stanford University

Authors

  • Christopher Thomas Williams

    Center for Turbulence Research, Stanford University

  • Mario Di Renzo

    University of Salento; Center for Turbulence Research, Stanford University, University of Salento

  • Marco Panesi

    University of Illinois at Urbana-Champaign

  • Parviz Moin

    Center for Turbulence Research, Stanford University, Stanford University